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