Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results

An edition of Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results (1969)

Flight measurements of the lift, longitudinal trim and drag of the Fairey Delta 2 at mach numbers up to 1.65 and comparisons with wind-tunnel results

By R. Rose

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Publish Date

1969

Publisher

H.M.S.O.

Language

eng

Pages

Description:

subjects: Airplanes, Drag (Aerodynamics), Flight testing, Lift (Aerodynamics), Triangular Wings, Fairey Delta (Supersonic plane), Airplanes, wings, Drag (aerodynamics)