Air Force Jayhawk
September 24th 03, 10:57 PM
On Wed, 24 Sep 2003 14:21:15 -0700, Hobo > wrote:
>
>
>It is commonly said that delta wing designs lose an above average amount
>of speed while turning and that this a deficiency of the design. Is this
>true, and if why does this occur? Also, how does this reputed flaw
>affect the potential performance of the Typhoon?
>
>TIA
Delta wings are typically a low aspect wing (stubby) which requires a
higher angle of attack to generate additionally lift than a higher
aspect (think Long and slim). Higher AOA results in higher drag,
hence one needs more thrust to maintian same speed.
I'm told that the F-106 was famous for it's first bat turn but after
that it was pretty much toast.
Ross "Roscoe" Dillon
USAF Flight Tester
(B-2, F-16, F-15, F-5, T-37, T-38, C-5, QF-106)
>
>
>It is commonly said that delta wing designs lose an above average amount
>of speed while turning and that this a deficiency of the design. Is this
>true, and if why does this occur? Also, how does this reputed flaw
>affect the potential performance of the Typhoon?
>
>TIA
Delta wings are typically a low aspect wing (stubby) which requires a
higher angle of attack to generate additionally lift than a higher
aspect (think Long and slim). Higher AOA results in higher drag,
hence one needs more thrust to maintian same speed.
I'm told that the F-106 was famous for it's first bat turn but after
that it was pretty much toast.
Ross "Roscoe" Dillon
USAF Flight Tester
(B-2, F-16, F-15, F-5, T-37, T-38, C-5, QF-106)