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
AirplanesDrag (Aerodynamics)Flight testingLift (Aerodynamics)Triangular WingsFairey Delta (Supersonic plane)Airplanes, wingsDrag (aerodynamics)
Writing a summary for young readers…
For young readers
Book data: Open Library