Engineer Jim wrote:
> The most complex ones that I worked with were the F-111 and the B-70. We
> tested inlet/engine combinations in the PWT Supersonic Wind Tunnel
> (16x16x40ft test section) to determine inlet performance at various Mach
> numbers. The desired characteristics of such inlets are high pressure
> recovery and freedom from inlet unstarts (where the shock system is expelled
> from the inlet).
I love this list.
AG
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