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originally posted by: zazen
originally posted by: weavty1
Refer here for the explanation...
www.abovetopsecret.com...
It's pretty damn cut and dry. No conspiracy here dude.
Well, yeah. I DID see the explanation by those who removed the post. If what was removed WERE something sensitive, wouldn't you expect them to do exactly as they did?
Also, the "DO NOT TALK ABOUT THIS" addendum doesn't exactly clear up the question.
I don't want to talk about the "banned member", just wondering what it was that was posted - you know, as part of the attempted "hoax".
Pretty cut and dry question, dude.
originally posted by: boomer135
a reply to: ThePeaceMaker
No it's not a real photo..its not designated as an f-19 and even the boneyard pics were proven to be faked.
originally posted by: MystikMushroom
a reply to: Astr0
I remember that plane...
I had a Testor's model of it when I was a little kiddo. I believe it was called a "stealth fighter". Interesting design, certainly ahead of it's time. In fact, it still looks "futuristic" 20+ odd years later!
originally posted by: mbkennel
originally posted by: MystikMushroom
a reply to: Astr0
I remember that plane...
I had a Testor's model of it when I was a little kiddo. I believe it was called a "stealth fighter". Interesting design, certainly ahead of it's time. In fact, it still looks "futuristic" 20+ odd years later!
Yeah, too bad the physics is wrong.
As you can see by visiting any aiport today, the wingtips need to be turned upwards to ameliorate the wingtip vortex.
And down is bad for rough landings too, one bounce and you'll scrape all that expensive paint off the tips and then Dad will be steaming mad.
More seriously, it sure looks like delta wings and triangles are what engineering says works.
Also I noticed that Hollywood "Aircraft" have canards on the same plane or lower as the main wing, but in actual aircraft, they're significantly higher and in uglier locations (e.g. typhoon, J-20
Source
North American Aviation (NAA) improved on the [plane's] basic concept by adding a set of drooping wing tip panels that were lowered at high speed. This helped trap the shock wave under the wing between the down-turned wing tips, and also added more vertical surface to the aircraft to improve directional stability at high speeds. NAA's solution had an additional advantage, as it decreased the surface area of the rear of the wing when the panels were moved into their high-speed position. This helped offset the rearward shift of the center of pressure, or "average lift point", with increasing speeds. Under normal conditions this caused an increasing nose-down trim, which had to be offset by moving the control surfaces, increasing drag. When the wing tips were drooped the surface area at the rear of the wings was lowered, moving the lift forward and counteracting this effect, reducing the need for control inputs.