shock bodies?
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shock bodies?
Can somebody pls tell me what exactly shock bodies are.Where they are located on the wing,what they look like,which a/c have them and what exactly they do?
I've been speaking to an engineer who claims they don't exist,but im sure they were covered in atpl studies.
Either way any thoughts appreciated.
Cheers.
I've been speaking to an engineer who claims they don't exist,but im sure they were covered in atpl studies.
Either way any thoughts appreciated.
Cheers.
Well, at last count I've done two aeronautics degrees and managed the certification of about a dozen aircraft types without hearing the term.
It sounds to me like one of those bits of terminology that somebody, somewhere, has invented and decided to include on a syllabus to make themselves seem cleverer than anybody else. I should either go back to your notes and see what they're going on about , or forget about it.
G
It sounds to me like one of those bits of terminology that somebody, somewhere, has invented and decided to include on a syllabus to make themselves seem cleverer than anybody else. I should either go back to your notes and see what they're going on about , or forget about it.
G
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mmm i guess im on dodgy ground then.Seem to remember they were related to something called the "area rule" and the "coke bottle effect" but can't remember more than that!
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Piper,
I understand that the term refers to a device designed to reduce the drag caused by the shock-wave which moves over a high-speed wing.
They were notably incorporated into the wing of the CV990 Coronado - visible as the four distinctive fairings mounted on the trailing edge, which also doubled as fuel tanks.
I understand that the term refers to a device designed to reduce the drag caused by the shock-wave which moves over a high-speed wing.
They were notably incorporated into the wing of the CV990 Coronado - visible as the four distinctive fairings mounted on the trailing edge, which also doubled as fuel tanks.
Usual disclaimers apply!
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Genghis
The Convair 990 had what's refered to as 'antishock bodies' on the wing.
Heres an article with reference about 2/3rds down
Damn you beat me to it KC
The Convair 990 had what's refered to as 'antishock bodies' on the wing.
Heres an article with reference about 2/3rds down
Damn you beat me to it KC
Ahhhhhhhhh,
So it's the use of shaped nacelles on the wings of a transonic aeroplane to optimise area ruling then.
Nope, still not heard the term until now, but the concept makes sense.
G
So it's the use of shaped nacelles on the wings of a transonic aeroplane to optimise area ruling then.
Nope, still not heard the term until now, but the concept makes sense.
G
Last edited by Genghis the Engineer; 3rd Sep 2005 at 12:03.
How about the Whitcomb Bodies on the Victor 2. IIRC the CV 990 bodies were on the upper surface whereas the Whitcomb Bodies on the Victor were lower surface mounted at about 1/3 span.
YS
YS
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I'm glad somebody can spell Kuchmann!. I was dying to add the name but, as Turin is bound to say I have enough trouble with English!
BTW Dr Kuchmann did lots of reserch at The Royal Aircraft Establishment at Farnborough, the home of british aviation.
Rgds Dr. I
BTW Dr Kuchmann did lots of reserch at The Royal Aircraft Establishment at Farnborough, the home of british aviation.
Rgds Dr. I
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Search for the Convair 990 on http://www.airliners.net/. There is a least one pic of a Spantax being dismantled where the term is used.
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