<?xml version="1.0" encoding="ISO-8859-1"?>
<rss version="2.0" xmlns:content="http://purl.org/rss/1.0/modules/content/">
<channel>
<title>sci.aeronautics</title>
<link>http://www.air-space.us/sci.aeronautics/22/1/</link>
<description>The science of aeronautics & related technology. (Moderated)</description>
<language>en-us</language>
<pubDate>Mon, 15 Mar 2010 23:27:02 -0400</pubDate>
<webMaster>info@air-space.us</webMaster>
<generator>http://www.air-space.us/</generator>
<docs>http://blogs.law.harvard.edu/tech/rss/</docs>
<item>
<title>Supersonic diffuser</title>
<link>http://www.air-space.us/sci.aeronautics/22/Supersonic-diffuser-article358.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Supersonic-diffuser-article358.htm</guid>
<description> igt; I want to design a supersonic diffuser for a supersonic wind tunnel. i/i igt; would like to know some bibliography about diffusser efficiency,/i igt; entrance angle, second throat length . Can anyone help me. Thanks/i igt;/i   Also look at Shapiros book on compressible fl ..</description>
<content:encoded><![CDATA[ igt; I want to design a supersonic diffuser for a supersonic wind tunnel. i/i igt; would like to know some bibliography about diffusser efficiency,/i igt; entrance angle, second throat length . Can anyone help me. Thanks/i igt;/i   Also look at Shapiros book on compressible fl ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:18:00 -0500</pubDate>
</item>
<item>
<title>Supersonic diffuser</title>
<link>http://www.air-space.us/sci.aeronautics/22/Supersonic-diffuser-article357.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Supersonic-diffuser-article357.htm</guid>
<description> igt; I want to design a supersonic diffuser for a supersonic wind tunnel. i/i igt; would like to know some bibliography about diffusser efficiency,/i igt; entrance angle, second throat length . Can anyone help me. Thanks/i igt;/i   There is some discussion about supersonic wind ..</description>
<content:encoded><![CDATA[ igt; I want to design a supersonic diffuser for a supersonic wind tunnel. i/i igt; would like to know some bibliography about diffusser efficiency,/i igt; entrance angle, second throat length . Can anyone help me. Thanks/i igt;/i   There is some discussion about supersonic wind ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:16:40 -0500</pubDate>
</item>
<item>
<title>Combining gearbox</title>
<link>http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article356.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article356.htm</guid>
<description> igt; Think normal car differential  with the power input at the wheel/i igt; shafts and power output at the quot;input shaftquot;./i igt; /i  Considering the sync portion of the question:  The problem here is to provide for load sharing without a tendency of  the two engines to  ..</description>
<content:encoded><![CDATA[ igt; Think normal car differential  with the power input at the wheel/i igt; shafts and power output at the quot;input shaftquot;./i igt; /i  Considering the sync portion of the question:  The problem here is to provide for load sharing without a tendency of  the two engines to  ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:14:18 -0500</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article355.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article355.htm</guid>
<description> igt; gt; And someone tell us how to explain how circulation induces lift/i igt; gt; to a budding pilot./i igt;/i igt; Track the path of a single air particle as the airfoil approaches and/i igt; passes.  It will move, roughly, in a circle (aka circulation).  A particle/i  ..</description>
<content:encoded><![CDATA[ igt; gt; And someone tell us how to explain how circulation induces lift/i igt; gt; to a budding pilot./i igt;/i igt; Track the path of a single air particle as the airfoil approaches and/i igt; passes.  It will move, roughly, in a circle (aka circulation).  A particle/i  ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:13:12 -0500</pubDate>
</item>
<item>
<title>About Spoilers on cars</title>
<link>http://www.air-space.us/sci.aeronautics/22/About-Spoilers-on-cars-article354.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/About-Spoilers-on-cars-article354.htm</guid>
<description> igt; what do you think about the spoilers mounted on the rear window/i igt; Id like to install one on my Audi A3 (for the aesthetics effect) but/i igt; Im insecure about his effect on boundary layer./i igt; Do you think it can raise the drag/i  Short answer: Yes.  The questi ..</description>
<content:encoded><![CDATA[ igt; what do you think about the spoilers mounted on the rear window/i igt; Id like to install one on my Audi A3 (for the aesthetics effect) but/i igt; Im insecure about his effect on boundary layer./i igt; Do you think it can raise the drag/i  Short answer: Yes.  The questi ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:12:03 -0500</pubDate>
</item>
<item>
<title>What is the difference between total and stagnation pressure?</title>
<link>http://www.air-space.us/sci.aeronautics/22/What-is-the-difference-between-total-and-stagnation-pressure-article353.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/What-is-the-difference-between-total-and-stagnation-pressure-article353.htm</guid>
<description> igt;  Im an aeronautical engineering student who is thoroughly confused/i igt; about the difference between total and stagnation pressures in a flow/i igt; (if any). When do we measure total pressure and when do we measure/i igt; stagnation pressure in a given flow Why do we nee ..</description>
<content:encoded><![CDATA[ igt;  Im an aeronautical engineering student who is thoroughly confused/i igt; about the difference between total and stagnation pressures in a flow/i igt; (if any). When do we measure total pressure and when do we measure/i igt; stagnation pressure in a given flow Why do we nee ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:11:14 -0500</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article352.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article352.htm</guid>
<description> igt;     My feeling is that there is no full circulation because it stops at the/i igt; stagnation points where there is upwash at the leading edge and downwash at/i igt; the trailing edge BECAUSE of Bernoullis theory, however Bernoullis theory/i igt; alone does not explain lift ..</description>
<content:encoded><![CDATA[ igt;     My feeling is that there is no full circulation because it stops at the/i igt; stagnation points where there is upwash at the leading edge and downwash at/i igt; the trailing edge BECAUSE of Bernoullis theory, however Bernoullis theory/i igt; alone does not explain lift ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:10:14 -0500</pubDate>
</item>
<item>
<title>American Society of Aeronautic Engineers</title>
<link>http://www.air-space.us/sci.aeronautics/22/American-Society-of-Aeronautic-Engineers-article351.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/American-Society-of-Aeronautic-Engineers-article351.htm</guid>
<description> I am researching professional societies in aeronautics.  I am aware of the start of the IAS in 193032, I was also aware that the SAE has an aerospace division.  In reading the history of the later, it turns out there was an American Society of Aeronautic Engineers that was merged in the SAE in 191 ..</description>
<content:encoded><![CDATA[ I am researching professional societies in aeronautics.  I am aware of the start of the IAS in 193032, I was also aware that the SAE has an aerospace division.  In reading the history of the later, it turns out there was an American Society of Aeronautic Engineers that was merged in the SAE in 191 ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:09:39 -0500</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article350.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article350.htm</guid>
<description> If you are able to get very close to the approach end of a runway serving heavy jets (727 and up) you can usually see the downwash effect on the smoke trail as the airplanes  quot;cross the fencequot;. AMAF if you can get very close to the centerline of the runway you can usually feel the downwas ..</description>
<content:encoded><![CDATA[ If you are able to get very close to the approach end of a runway serving heavy jets (727 and up) you can usually see the downwash effect on the smoke trail as the airplanes  quot;cross the fencequot;. AMAF if you can get very close to the centerline of the runway you can usually feel the downwas ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:08:51 -0500</pubDate>
</item>
<item>
<title>About Spoilers on cars</title>
<link>http://www.air-space.us/sci.aeronautics/22/About-Spoilers-on-cars-article349.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/About-Spoilers-on-cars-article349.htm</guid>
<description> igt; what do you think about the spoilers mounted on the rear window/i igt; Id like to install one on my Audi A3 (for the aesthetics effect) but/i igt; Im insecure about his effect on boundary layer./i igt; Do you think it can raise the drag/i  Maybe, maybe not.  The devil i ..</description>
<content:encoded><![CDATA[ igt; what do you think about the spoilers mounted on the rear window/i igt; Id like to install one on my Audi A3 (for the aesthetics effect) but/i igt; Im insecure about his effect on boundary layer./i igt; Do you think it can raise the drag/i  Maybe, maybe not.  The devil i ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:08:11 -0500</pubDate>
</item>
<item>
<title>UAV's</title>
<link>http://www.air-space.us/sci.aeronautics/22/UAVs-article348.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/UAVs-article348.htm</guid>
<description> igt; Can anyone recommend me any book on UAV design or guide to build/i igt; one from scratch or experience doing them starting from the sizing/i igt; equations to the final prototype Thanks/i igt; /i   The laws of aerodynamics do not change depending on whether there is a  pi ..</description>
<content:encoded><![CDATA[ igt; Can anyone recommend me any book on UAV design or guide to build/i igt; one from scratch or experience doing them starting from the sizing/i igt; equations to the final prototype Thanks/i igt; /i   The laws of aerodynamics do not change depending on whether there is a  pi ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:07:29 -0500</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article347.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article347.htm</guid>
<description> igt;     I choose not to teach the circulation theory to my students because I/i igt; dont think it exists in the manner the term suggests it does.  I understand/i igt; what people are trying to explain by using the term quot;circulationquot; (basically/i igt; upwash and downwa ..</description>
<content:encoded><![CDATA[ igt;     I choose not to teach the circulation theory to my students because I/i igt; dont think it exists in the manner the term suggests it does.  I understand/i igt; what people are trying to explain by using the term quot;circulationquot; (basically/i igt; upwash and downwa ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:06:54 -0500</pubDate>
</item>
<item>
<title>Kutta-Joukowski theorem in compressible flow</title>
<link>http://www.air-space.us/sci.aeronautics/22/KuttaJoukowski-theorem-in-compressible-flow-article346.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/KuttaJoukowski-theorem-in-compressible-flow-article346.htm</guid>
<description> Is Kutta Joukowski theorem still applicable in compressible (subsonic) flow  In other words, does the same circulation produces the same lift at 0.2 and  0.8 mach (V being the same, of course)   Marco     </description>
<content:encoded><![CDATA[ Is Kutta Joukowski theorem still applicable in compressible (subsonic) flow  In other words, does the same circulation produces the same lift at 0.2 and  0.8 mach (V being the same, of course)   Marco     ]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:06:06 -0500</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article345.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article345.htm</guid>
<description> igt;    I choose not to teach the circulation theory to my students because I/i igt; dont think it exists in the manner the term suggests it does.  I /i igt; understand/i igt; what people are trying to explain by using the term quot;circulationquot; /i igt; (basically/i  ..</description>
<content:encoded><![CDATA[ igt;    I choose not to teach the circulation theory to my students because I/i igt; dont think it exists in the manner the term suggests it does.  I /i igt; understand/i igt; what people are trying to explain by using the term quot;circulationquot; /i igt; (basically/i  ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:05:23 -0500</pubDate>
</item>
<item>
<title>Jet engine noise suppressor</title>
<link>http://www.air-space.us/sci.aeronautics/22/Jet-engine-noise-suppressor-article344.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Jet-engine-noise-suppressor-article344.htm</guid>
<description> igt; Can anyone tell me how a noise suppressor for a turbojet engine works/i  Most of the noise from a turbojet comes from shearing between the highspeed  hot exhaust jet and the stationary cool ambient air.  Most of the noise  suppressors (aka hushkits) are designed to promote rapid mixing ..</description>
<content:encoded><![CDATA[ igt; Can anyone tell me how a noise suppressor for a turbojet engine works/i  Most of the noise from a turbojet comes from shearing between the highspeed  hot exhaust jet and the stationary cool ambient air.  Most of the noise  suppressors (aka hushkits) are designed to promote rapid mixing ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:04:39 -0500</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article343.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article343.htm</guid>
<description> igt;Unfortunately, there IS no simple explanation of the effect of airfoil/i igt;camber without getting into advanced fluid mechanics and differential/i igt;equations.  I liked the explanation of a former sci.aero moderator,/i igt;Mary Shafer action of the quot;lift daemonsquot ..</description>
<content:encoded><![CDATA[ igt;Unfortunately, there IS no simple explanation of the effect of airfoil/i igt;camber without getting into advanced fluid mechanics and differential/i igt;equations.  I liked the explanation of a former sci.aero moderator,/i igt;Mary Shafer action of the quot;lift daemonsquot ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:04:00 -0500</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article342.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article342.htm</guid>
<description> igt;gt; And someone tell us how to explain how circulation induces lift/i igt;gt; to a budding pilot./i .... igt;A particle /i igt;going over the wing will initially move forward and up due to positive /i igt;pressure from the leading edge, then get pulled back and down /i ..</description>
<content:encoded><![CDATA[ igt;gt; And someone tell us how to explain how circulation induces lift/i igt;gt; to a budding pilot./i .... igt;A particle /i igt;going over the wing will initially move forward and up due to positive /i igt;pressure from the leading edge, then get pulled back and down /i ..]]></content:encoded>
<pubDate>Tue, 30 Jan 2007 21:03:17 -0500</pubDate>
</item>
<item>
<title>Circulation control technique</title>
<link>http://www.air-space.us/sci.aeronautics/22/Circulation-control-technique-article341.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Circulation-control-technique-article341.htm</guid>
<description> I have just done my Msc thesis on circulation control of a marine propeller duct.  It also proposes a new type of non ducted propeller that can utilise the effect.  It may be of interest to some people now or in the future so just in case anyone is interested you can find it here:  http://www.geoci ..</description>
<content:encoded><![CDATA[ I have just done my Msc thesis on circulation control of a marine propeller duct.  It also proposes a new type of non ducted propeller that can utilise the effect.  It may be of interest to some people now or in the future so just in case anyone is interested you can find it here:  http://www.geoci ..]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:27:11 -0500</pubDate>
</item>
<item>
<title>Combining gearbox</title>
<link>http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article340.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article340.htm</guid>
<description> Think normal car differential  with the power input at the wheel shafts and power output at the quot;input shaftquot;.  </description>
<content:encoded><![CDATA[ Think normal car differential  with the power input at the wheel shafts and power output at the quot;input shaftquot;.  ]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:26:02 -0500</pubDate>
</item>
<item>
<title>Aircraft simulation software</title>
<link>http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article339.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article339.htm</guid>
<description> I use a commercial flight simulator that is also available for home use. It is call Xplane and is developed by Austin Meyer.  It comes with quot;planemakerquot; software, and if you know the drag coefficient of the components, you can put them in easily.  Adam  </description>
<content:encoded><![CDATA[ I use a commercial flight simulator that is also available for home use. It is call Xplane and is developed by Austin Meyer.  It comes with quot;planemakerquot; software, and if you know the drag coefficient of the components, you can put them in easily.  Adam  ]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:24:21 -0500</pubDate>
</item>
<item>
<title>About Spoilers on cars</title>
<link>http://www.air-space.us/sci.aeronautics/22/About-Spoilers-on-cars-article338.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/About-Spoilers-on-cars-article338.htm</guid>
<description> Hi, what do you think about the spoilers mounted on the rear window Id like to install one on my Audi A3 (for the aesthetics effect) but Im insecure about his effect on boundary layer. Do you think it can raise the drag Thanks.  Francesco. Italy.  </description>
<content:encoded><![CDATA[ Hi, what do you think about the spoilers mounted on the rear window Id like to install one on my Audi A3 (for the aesthetics effect) but Im insecure about his effect on boundary layer. Do you think it can raise the drag Thanks.  Francesco. Italy.  ]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:23:18 -0500</pubDate>
</item>
<item>
<title>Aircraft simulation software</title>
<link>http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article337.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article337.htm</guid>
<description> igt; Can anyone suggest aerodynamics simulation software that will allow me/i igt; to simulate the entire aircraft (and not just airfoil) including/i igt; fuselage, wings, tail, canards, etc.  In essence, I want to design a/i igt; 3D aircraft using this tool and then simulate it ..</description>
<content:encoded><![CDATA[ igt; Can anyone suggest aerodynamics simulation software that will allow me/i igt; to simulate the entire aircraft (and not just airfoil) including/i igt; fuselage, wings, tail, canards, etc.  In essence, I want to design a/i igt; 3D aircraft using this tool and then simulate it ..]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:21:34 -0500</pubDate>
</item>
<item>
<title>Jet engine noise suppressor</title>
<link>http://www.air-space.us/sci.aeronautics/22/Jet-engine-noise-suppressor-article336.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Jet-engine-noise-suppressor-article336.htm</guid>
<description> Can anyone tell me how a noise suppressor for a turbojet engine works  </description>
<content:encoded><![CDATA[ Can anyone tell me how a noise suppressor for a turbojet engine works  ]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:20:11 -0500</pubDate>
</item>
<item>
<title>UAV's</title>
<link>http://www.air-space.us/sci.aeronautics/22/UAVs-article335.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/UAVs-article335.htm</guid>
<description> Can anyone recommend me any book on UAV design or guide to build one from scratch or experience doing them starting from the sizing equations to the final prototype Thanks  </description>
<content:encoded><![CDATA[ Can anyone recommend me any book on UAV design or guide to build one from scratch or experience doing them starting from the sizing equations to the final prototype Thanks  ]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:19:35 -0500</pubDate>
</item>
<item>
<title>Aircraft simulation software</title>
<link>http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article334.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article334.htm</guid>
<description>  igt; Can anyone suggest aerodynamics simulation software that will allow me/i igt; to simulate the entire aircraft (and not just airfoil) including/i igt; fuselage, wings, tail, canards, etc.  In essence, I want to design a/i igt; 3D aircraft using this tool and then simulate it ..</description>
<content:encoded><![CDATA[  igt; Can anyone suggest aerodynamics simulation software that will allow me/i igt; to simulate the entire aircraft (and not just airfoil) including/i igt; fuselage, wings, tail, canards, etc.  In essence, I want to design a/i igt; 3D aircraft using this tool and then simulate it ..]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:18:17 -0500</pubDate>
</item>
<item>
<title>Supersonic diffuser</title>
<link>http://www.air-space.us/sci.aeronautics/22/Supersonic-diffuser-article333.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Supersonic-diffuser-article333.htm</guid>
<description> I want to design a supersonic diffuser for a supersonic wind tunnel. i would like to know some bibliography about diffusser efficiency, entrance angle, second throat length . Can anyone help me. Thanks  </description>
<content:encoded><![CDATA[ I want to design a supersonic diffuser for a supersonic wind tunnel. i would like to know some bibliography about diffusser efficiency, entrance angle, second throat length . Can anyone help me. Thanks  ]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:17:00 -0500</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article332.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article332.htm</guid>
<description> igt; Someone tell us how to explain how circulation induces lift/i igt; to a budding pilot. Bernoulli is easier to understand and demonstrate./i igt; Oh, yeah, FWIW, a supercritical wing produces lift because its at an/i igt; angle of attack, just like a symmetrical or plane surf ..</description>
<content:encoded><![CDATA[ igt; Someone tell us how to explain how circulation induces lift/i igt; to a budding pilot. Bernoulli is easier to understand and demonstrate./i igt; Oh, yeah, FWIW, a supercritical wing produces lift because its at an/i igt; angle of attack, just like a symmetrical or plane surf ..]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:16:26 -0500</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article331.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article331.htm</guid>
<description> igt; Well. I cant add to the Bernoulli discussion because its over 30 days/i igt; old or has been closed by the moderator. (Remove it from the list,/i igt; then). And someone tell us how to explain how circulation induces lift/i igt; to a budding pilot. Bernoulli is easier to un ..</description>
<content:encoded><![CDATA[ igt; Well. I cant add to the Bernoulli discussion because its over 30 days/i igt; old or has been closed by the moderator. (Remove it from the list,/i igt; then). And someone tell us how to explain how circulation induces lift/i igt; to a budding pilot. Bernoulli is easier to un ..]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:15:16 -0500</pubDate>
</item>
<item>
<title>The wrong &quot;Bernoulli&quot; explanation in Sci. American for April 2005</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article330.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article330.htm</guid>
<description> igt; Flowwise Circulation is a pure mathematical model, for correcting the/i igt; Potential flow field/i igt;/i igt; Its very easy to see that in real flight there is no flowwise/i igt; circulation around the wing, only the spanwise circulation in/i igt; connection wit ..</description>
<content:encoded><![CDATA[ igt; Flowwise Circulation is a pure mathematical model, for correcting the/i igt; Potential flow field/i igt;/i igt; Its very easy to see that in real flight there is no flowwise/i igt; circulation around the wing, only the spanwise circulation in/i igt; connection wit ..]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:14:35 -0500</pubDate>
</item>
<item>
<title>A340</title>
<link>http://www.air-space.us/sci.aeronautics/22/A340-article329.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/A340-article329.htm</guid>
<description> igt; Do you have any recommended website or text book about A340,/i igt; particularly about its wing structure. i am a student who is doing/i igt; about wing structure of A340. Thank you for your helps....../i  What do you need to know about it  Airbus uses pretty much the same  str ..</description>
<content:encoded><![CDATA[ igt; Do you have any recommended website or text book about A340,/i igt; particularly about its wing structure. i am a student who is doing/i igt; about wing structure of A340. Thank you for your helps....../i  What do you need to know about it  Airbus uses pretty much the same  str ..]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:13:39 -0500</pubDate>
</item>
<item>
<title>Aircraft simulation software</title>
<link>http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article328.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article328.htm</guid>
<description> igt; Can anyone suggest aerodynamics simulation software that will allow me/i igt; to simulate the entire aircraft (and not just airfoil) including/i igt; fuselage, wings, tail, canards, etc.  In essence, I want to design a/i igt; 3D aircraft using this tool and then simulate it ..</description>
<content:encoded><![CDATA[ igt; Can anyone suggest aerodynamics simulation software that will allow me/i igt; to simulate the entire aircraft (and not just airfoil) including/i igt; fuselage, wings, tail, canards, etc.  In essence, I want to design a/i igt; 3D aircraft using this tool and then simulate it ..]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:06:25 -0500</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article327.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article327.htm</guid>
<description> igt; And someone tell us how to explain how circulation induces lift/i igt; to a budding pilot./i  Track the path of a single air particle as the airfoil approaches and  passes.  It will move, roughly, in a circle (aka circulation).  A particle  going over the wing will initially move for ..</description>
<content:encoded><![CDATA[ igt; And someone tell us how to explain how circulation induces lift/i igt; to a budding pilot./i  Track the path of a single air particle as the airfoil approaches and  passes.  It will move, roughly, in a circle (aka circulation).  A particle  going over the wing will initially move for ..]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:05:49 -0500</pubDate>
</item>
<item>
<title>Aircraft simulation software</title>
<link>http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article326.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article326.htm</guid>
<description> igt; Can anyone suggest aerodynamics simulation software that will allow me/i igt; to simulate the entire aircraft (and not just airfoil) including/i igt; fuselage, wings, tail, canards, etc.  In essence, I want to design a/i igt; 3D aircraft using this tool and then simulate it ..</description>
<content:encoded><![CDATA[ igt; Can anyone suggest aerodynamics simulation software that will allow me/i igt; to simulate the entire aircraft (and not just airfoil) including/i igt; fuselage, wings, tail, canards, etc.  In essence, I want to design a/i igt; 3D aircraft using this tool and then simulate it ..]]></content:encoded>
<pubDate>Mon, 11 Dec 2006 13:05:08 -0500</pubDate>
</item>
<item>
<title>Saab's early regional jet design of 60s - 70s</title>
<link>http://www.air-space.us/sci.aeronautics/22/Saabs-early-regional-jet-design-of-60s--70s-article322.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Saabs-early-regional-jet-design-of-60s--70s-article322.htm</guid>
<description> A couple of months ago I saw a web page giving information about an early regional jet project of Saab aircraft. Even there was a drawing of the projected aircraft. For the last two days, Ive been searching for the same site and other web sites regarding Saabs early regional jet design, but I am  ..</description>
<content:encoded><![CDATA[ A couple of months ago I saw a web page giving information about an early regional jet project of Saab aircraft. Even there was a drawing of the projected aircraft. For the last two days, Ive been searching for the same site and other web sites regarding Saabs early regional jet design, but I am  ..]]></content:encoded>
<pubDate>Tue, 10 Oct 2006 17:53:19 -0400</pubDate>
</item>
<item>
<title>The Wronger Bernoulli etc</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article321.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-Wronger-Bernoulli-etc-article321.htm</guid>
<description> Well. I cant add to the Bernoulli discussion because its over 30 days old or has been closed by the moderator. (Remove it from the list, then). And someone tell us how to explain how circulation induces lift to a budding pilot. Bernoulli is easier to understand and demonstrate. Oh, yeah, FWIW, a  ..</description>
<content:encoded><![CDATA[ Well. I cant add to the Bernoulli discussion because its over 30 days old or has been closed by the moderator. (Remove it from the list, then). And someone tell us how to explain how circulation induces lift to a budding pilot. Bernoulli is easier to understand and demonstrate. Oh, yeah, FWIW, a  ..]]></content:encoded>
<pubDate>Tue, 10 Oct 2006 17:52:42 -0400</pubDate>
</item>
<item>
<title>Aircraft simulation software</title>
<link>http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article320.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Aircraft-simulation-software-article320.htm</guid>
<description> Can anyone suggest aerodynamics simulation software that will allow me to simulate the entire aircraft (and not just airfoil) including fuselage, wings, tail, canards, etc.  In essence, I want to design a 3D aircraft using this tool and then simulate its flight dynamics to see if it is airworthy ..</description>
<content:encoded><![CDATA[ Can anyone suggest aerodynamics simulation software that will allow me to simulate the entire aircraft (and not just airfoil) including fuselage, wings, tail, canards, etc.  In essence, I want to design a 3D aircraft using this tool and then simulate its flight dynamics to see if it is airworthy ..]]></content:encoded>
<pubDate>Tue, 10 Oct 2006 17:51:07 -0400</pubDate>
</item>
<item>
<title>Combining gearbox</title>
<link>http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article319.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article319.htm</guid>
<description> igt; is there any information about combining gearboxes. If two engines/i igt; power say one rotor how can this be acomplished without total/i igt; synchronization of the engines/i igt;/i igt; Thanks a lot/i igt; Achilleas/i       I seem to recall our X18 VTOL at Edw ..</description>
<content:encoded><![CDATA[ igt; is there any information about combining gearboxes. If two engines/i igt; power say one rotor how can this be acomplished without total/i igt; synchronization of the engines/i igt;/i igt; Thanks a lot/i igt; Achilleas/i       I seem to recall our X18 VTOL at Edw ..]]></content:encoded>
<pubDate>Tue, 10 Oct 2006 17:50:26 -0400</pubDate>
</item>
<item>
<title>A340</title>
<link>http://www.air-space.us/sci.aeronautics/22/A340-article318.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/A340-article318.htm</guid>
<description> Do you have any recommended website or text book about A340, particularly about its wing structure. i am a student who is doing about wing structure of A340. Thank you for your helps......  </description>
<content:encoded><![CDATA[ Do you have any recommended website or text book about A340, particularly about its wing structure. i am a student who is doing about wing structure of A340. Thank you for your helps......  ]]></content:encoded>
<pubDate>Tue, 10 Oct 2006 17:11:58 -0400</pubDate>
</item>
<item>
<title>Combining gearbox</title>
<link>http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article317.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article317.htm</guid>
<description> igt; gt; is there any information about combining gearboxes. If two engines/i igt; gt; power say one rotor how can this be acomplished without total/i igt; gt; synchronization of the engines/i igt; /i igt; The strength of the shafts automatically quot;synchronizesquot;  ..</description>
<content:encoded><![CDATA[ igt; gt; is there any information about combining gearboxes. If two engines/i igt; gt; power say one rotor how can this be acomplished without total/i igt; gt; synchronization of the engines/i igt; /i igt; The strength of the shafts automatically quot;synchronizesquot;  ..]]></content:encoded>
<pubDate>Tue, 10 Oct 2006 17:11:29 -0400</pubDate>
</item>
<item>
<title>The wrong &quot;Bernoulli&quot; explanation in Sci. American for April 2005</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article316.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article316.htm</guid>
<description> igt; gt; All new airliners of Airbus or Boeing make and all top bizjets, have/i igt; gt; low drag quot;supercritical wingsquot;, with almost flat upper surface and/i igt; gt; curved lower surface (to host wing beam and fuel)/i igt; gt;/i igt; gt; I have never seen Sci ..</description>
<content:encoded><![CDATA[ igt; gt; All new airliners of Airbus or Boeing make and all top bizjets, have/i igt; gt; low drag quot;supercritical wingsquot;, with almost flat upper surface and/i igt; gt; curved lower surface (to host wing beam and fuel)/i igt; gt;/i igt; gt; I have never seen Sci ..]]></content:encoded>
<pubDate>Tue, 10 Oct 2006 17:10:48 -0400</pubDate>
</item>
<item>
<title>The wrong &quot;Bernoulli&quot; explanation in Sci. American for April 2005</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article315.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article315.htm</guid>
<description> igt; gt; All new airliners of Airbus or Boeing make and all top bizjets, have/i igt; gt; low drag quot;supercritical wingsquot;, with almost flat upper surface and/i igt; gt; curved lower surface (to host wing beam and fuel)/i igt; gt;/i igt; gt; I have never seen Sci ..</description>
<content:encoded><![CDATA[ igt; gt; All new airliners of Airbus or Boeing make and all top bizjets, have/i igt; gt; low drag quot;supercritical wingsquot;, with almost flat upper surface and/i igt; gt; curved lower surface (to host wing beam and fuel)/i igt; gt;/i igt; gt; I have never seen Sci ..]]></content:encoded>
<pubDate>Tue, 10 Oct 2006 17:09:58 -0400</pubDate>
</item>
<item>
<title>The wrong &quot;Bernoulli&quot; explanation in Sci. American for April 2005</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article314.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article314.htm</guid>
<description> igt; Bernoulli equation seems to very misunderstod by americans, even/i igt; respected universities and Professors should know better about the/i igt; physics/i       Everybody seems to want to be an aerodynamicist, and explain Bernoullis Theorem.  See todays quot;Overboardquot; ..</description>
<content:encoded><![CDATA[ igt; Bernoulli equation seems to very misunderstod by americans, even/i igt; respected universities and Professors should know better about the/i igt; physics/i       Everybody seems to want to be an aerodynamicist, and explain Bernoullis Theorem.  See todays quot;Overboardquot; ..]]></content:encoded>
<pubDate>Wed, 23 Aug 2006 14:16:38 -0400</pubDate>
</item>
<item>
<title>The wrong &quot;Bernoulli&quot; explanation in Sci. American for April 2005</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article313.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article313.htm</guid>
<description> igt; gt; gt; A recent issue of Scientific American carries a mind virus :)/i igt; gt; gt;/i igt; gt; gt; In the quot;Working Knowledgequot; column, the author presents an incorrect and/i igt; gt; gt; longdebunked explanation of how wings work:/i igt; gt; gt;/i ..</description>
<content:encoded><![CDATA[ igt; gt; gt; A recent issue of Scientific American carries a mind virus :)/i igt; gt; gt;/i igt; gt; gt; In the quot;Working Knowledgequot; column, the author presents an incorrect and/i igt; gt; gt; longdebunked explanation of how wings work:/i igt; gt; gt;/i ..]]></content:encoded>
<pubDate>Wed, 23 Aug 2006 14:15:22 -0400</pubDate>
</item>
<item>
<title>The wrong &quot;Bernoulli&quot; explanation in Sci. American for April 2005</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article312.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article312.htm</guid>
<description> igt; All new airliners of Airbus or Boeing make and all top bizjets, have/i igt; low drag quot;supercritical wingsquot;, with almost flat upper surface and/i igt; curved lower surface (to host wing beam and fuel)/i igt;/i igt; I have never seen Scientific American explain  ..</description>
<content:encoded><![CDATA[ igt; All new airliners of Airbus or Boeing make and all top bizjets, have/i igt; low drag quot;supercritical wingsquot;, with almost flat upper surface and/i igt; curved lower surface (to host wing beam and fuel)/i igt;/i igt; I have never seen Scientific American explain  ..]]></content:encoded>
<pubDate>Wed, 23 Aug 2006 14:05:27 -0400</pubDate>
</item>
<item>
<title>Combining gearbox</title>
<link>http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article311.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article311.htm</guid>
<description> igt;is there any information about combining gearboxes. If two engines/i igt;power say one rotor how can this be acomplished without total/i igt;synchronization of the engines/i  A limited slip diff with a freerwheel, one idly supposes  Brian Whatcott    Altus OK  </description>
<content:encoded><![CDATA[ igt;is there any information about combining gearboxes. If two engines/i igt;power say one rotor how can this be acomplished without total/i igt;synchronization of the engines/i  A limited slip diff with a freerwheel, one idly supposes  Brian Whatcott    Altus OK  ]]></content:encoded>
<pubDate>Wed, 23 Aug 2006 14:04:39 -0400</pubDate>
</item>
<item>
<title>Combining gearbox</title>
<link>http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article310.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article310.htm</guid>
<description> igt; is there any information about combining gearboxes. If two engines/i igt; power say one rotor how can this be acomplished without total/i igt; synchronization of the engines/i  The strength of the shafts automatically quot;synchronizesquot; the engines. The engines cannot tur ..</description>
<content:encoded><![CDATA[ igt; is there any information about combining gearboxes. If two engines/i igt; power say one rotor how can this be acomplished without total/i igt; synchronization of the engines/i  The strength of the shafts automatically quot;synchronizesquot; the engines. The engines cannot tur ..]]></content:encoded>
<pubDate>Wed, 23 Aug 2006 14:03:55 -0400</pubDate>
</item>
<item>
<title>Combining gearbox</title>
<link>http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article309.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/Combining-gearbox-article309.htm</guid>
<description> Hello there,  is there any information about combining gearboxes. If two engines power say one rotor how can this be acomplished without total synchronization of the engines  Thanks a lot Achilleas  </description>
<content:encoded><![CDATA[ Hello there,  is there any information about combining gearboxes. If two engines power say one rotor how can this be acomplished without total synchronization of the engines  Thanks a lot Achilleas  ]]></content:encoded>
<pubDate>Tue, 08 Aug 2006 11:53:15 -0400</pubDate>
</item>
<item>
<title>The wrong &quot;Bernoulli&quot; explanation in Sci. American for April 2005</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article308.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article308.htm</guid>
<description> igt; gt; A recent issue of Scientific American carries a mind virus :)/i igt; gt;/i igt; gt; In the quot;Working Knowledgequot; column, the author presents an incorrect and/i igt; gt; longdebunked explanation of how wings work:/i igt; gt;/i igt; gt; quot;becau ..</description>
<content:encoded><![CDATA[ igt; gt; A recent issue of Scientific American carries a mind virus :)/i igt; gt;/i igt; gt; In the quot;Working Knowledgequot; column, the author presents an incorrect and/i igt; gt; longdebunked explanation of how wings work:/i igt; gt;/i igt; gt; quot;becau ..]]></content:encoded>
<pubDate>Tue, 08 Aug 2006 11:52:40 -0400</pubDate>
</item>
<item>
<title>The wrong &quot;Bernoulli&quot; explanation in Sci. American for April 2005</title>
<link>http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article307.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/The-wrong-quotBernoulliquot-explanation-in-Sci-American-for-April-2005-article307.htm</guid>
<description> Some interesting info for interested readers:  http://user.unifrankfurt.de/weltner/Flight/PHYSIC4.htm http://user.unifrankfurt.de/weltner/Mis6/mis6.html http://amasci.com/wing/airfoil.html http://www.aa.washington.edu/faculty/eberhardt/lift.htm  </description>
<content:encoded><![CDATA[ Some interesting info for interested readers:  http://user.unifrankfurt.de/weltner/Flight/PHYSIC4.htm http://user.unifrankfurt.de/weltner/Mis6/mis6.html http://amasci.com/wing/airfoil.html http://www.aa.washington.edu/faculty/eberhardt/lift.htm  ]]></content:encoded>
<pubDate>Tue, 08 Aug 2006 11:51:52 -0400</pubDate>
</item>
<item>
<title>X-29</title>
<link>http://www.air-space.us/sci.aeronautics/22/X29-article306.htm</link>
<guid isPermaLink="true">http://www.air-space.us/sci.aeronautics/22/X29-article306.htm</guid>
<description> igt; Does anyone know if it was Lear or Honeywell who built the flight/i igt; control computers for the X29 /i  Pretty sure it was Honeywell.  I was working at Honeywell at the time and the company made a big thing about it.  </description>
<content:encoded><![CDATA[ igt; Does anyone know if it was Lear or Honeywell who built the flight/i igt; control computers for the X29 /i  Pretty sure it was Honeywell.  I was working at Honeywell at the time and the company made a big thing about it.  ]]></content:encoded>
<pubDate>Tue, 08 Aug 2006 11:51:20 -0400</pubDate>
</item>
</channel>
</rss>