Aeronautical study of a wing-fuselage combination employing a wing swept back 63 degrees : characteristics at supersonic speeds of a model with the wing twisted and cambered for uniform load

Hall, Charles F Heitmeyer, John C
naca-rm-a9j24
January 09, 1950


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1950/naca-rm-a9j24.pdf