Tests have been made at Mach numbers up to 0.93 in the Royal Aircraft Establishment 10 ft X 7 ft High Speed Wind Tunnel to examine how the longitudinal characteristics of a fighter-type aircraft are affected by the ...
The longitudinal characteristics of the aircraft (Aspect Ratio 4.0) were investigated on a half-model in the Royal Aircraft Establishment 10 ft × 7It Wind Tunnel at a Reynolds number of 1.3 million up to a Mach number of ...