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#1
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A while back I read an FAA definition of a glider (as
opposed to an airplane). I think it was an FAA document that referenced JAR 22. One of the criteria was a span squared over weight number (S^2/W). I can't find this document. Does this sound familiar to anyone? Bob C. |
#2
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Bob,
Here is the reference: http://mysite.verizon.net/engreenwel...teria_2004.pdf You have it backward it is Weight / span ^ 2 0.62 Wayne HP-14 "6F" http://www.soaridaho.com/Schreder "Bob C" wrote in message ... A while back I read an FAA definition of a glider (as opposed to an airplane). I think it was an FAA document that referenced JAR 22. One of the criteria was a span squared over weight number (S^2/W). I can't find this document. Does this sound familiar to anyone? Bob C. |
#3
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Thanks. I found it online about two minutes after
I posted the question. Advisory Circular 21.17-2A Bob C. At 03:36 29 April 2007, Wayne Paul wrote: Bob, Here is the reference: http://mysite.verizon.net/engreenwel...r_criteria_200 4.pdf You have it backward it is Weight / span ^ 2 wrote in message ... A while back I read an FAA definition of a glider (as opposed to an airplane). I think it was an FAA document that referenced JAR 22. One of the criteria was a span squared over weight number (S^2/W). I can't find this document. Does this sound familiar to anyone? Bob C. |
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On Sat, 28 Apr 2007 21:32:47 -0600, "Wayne Paul"
wrote: Bob, Here is the reference: http://mysite.verizon.net/engreenwel...teria_2004.pdf You have it backward it is Weight / span ^ 2 0.62 In other words, it's the wing loading. rj |
#5
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![]() "Ralph Jones" wrote in message ... On Sat, 28 Apr 2007 21:32:47 -0600, "Wayne Paul" wrote: Bob, Here is the reference: http://mysite.verizon.net/engreenwel...teria_2004.pdf You have it backward it is Weight / span ^ 2 0.62 In other words, it's the wing loading. Ralph, No, wing loading = weight / (span * MAC). Span loading does not consider the wing's cord. Wayne HP-14 "6F" http://www.soaridaho.com/Schreder .. |
#6
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On Sun, 29 Apr 2007 12:25:49 -0600, "Wayne Paul"
wrote: "Ralph Jones" wrote in message .. . On Sat, 28 Apr 2007 21:32:47 -0600, "Wayne Paul" wrote: Bob, Here is the reference: http://mysite.verizon.net/engreenwel...teria_2004.pdf You have it backward it is Weight / span ^ 2 0.62 In other words, it's the wing loading. Ralph, No, wing loading = weight / (span * MAC). Span loading does not consider the wing's cord. Oops, my bad. rj |
#7
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Isn't a glider simply defined as an aircraft with no
motive power..? Any aircraft can become a 'glider', whereas a sailplane is a glider built specifically for soaring. What a motorglider is, I have no idea... ;o) At 03:24 29 April 2007, Bob C wrote: A while back I read an FAA definition of a glider (as opposed to an airplane). I think it was an FAA document that referenced JAR 22. One of the criteria was a span squared over weight number (S^2/W). I can't find this document. Does this sound familiar to anyone? Bob C. There are only 10 types of people in the world. Those who understand Binary, and those who don't. |
#8
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Al,
In the US formula is used to determine whether a fixed wing aircraft with an engine is classified as a glider or as an airplane. Wayne HP-14 "6F" http://www.soaridaho.com/ "Al Eddie" wrote in message ... Isn't a glider simply defined as an aircraft with no motive power..? Any aircraft can become a 'glider', whereas a sailplane is a glider built specifically for soaring. What a motorglider is, I have no idea... ;o) At 03:24 29 April 2007, Bob C wrote: A while back I read an FAA definition of a glider (as opposed to an airplane). I think it was an FAA document that referenced JAR 22. One of the criteria was a span squared over weight number (S^2/W). I can't find this document. Does this sound familiar to anyone? Bob C. There are only 10 types of people in the world. Those who understand Binary, and those who don't. |
#9
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Boy, this is how years worth of misconceptions get started..
If you go to the FAA website http://www.FAA.gov and use the aircraft certification site ... reference the FAR part 1 Definitions. http://www.airweb.faa.gov/Regulatory...2572960077077A page 8 states " Glider means a heavier - than - air aircraft, that is supported in flight by the dynamic reaction of the air against its lifting surfaces and whose free flight does not depend principally on an engine." The JAR 22 reference is a European reference. CAR 3 is the old certification reference for the USA. I can't recall any US gliders that have been certified recently. The Kansas City Small Aircraft Directorate is in charge of that in the US. In fact, when I started to register my ASW-20 they were going to register it as an LSA (light Sport Aircraft) until I told then the top speed is 160K ! "Wing Loading"is Weight/Wing Area (typically ASW-20 is 110 sq ft approx.) "Span Loading" is the distribution of lift over the wing span, is typically elliptical (ie. is the top part of an ellipse with the greatest amount at the center, decreasing 'elliptically' to the tip). |
#10
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At 12:42 30 April 2007, Wayne Paul wrote:
Al, In the US formula is used to determine whether a fixed wing aircraft with an engine is classified as a glider or as an airplane. Wayne HP-14 '6F' http://www.soaridaho.com/ All very well but, when the engine(s) fail(s), no number of formulae will ever determine that aircraft to be anything other than a glider... ;o) |
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