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Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45©� sweptback highly tapered wing in combination with basic and indented bodies

Published Year

• 1950-1959 (1)

Subject

• Aerodynamic load (1)
• Aerofoils--Testing (1)
• Airplanes--Fuselage (1)
• Airplanes--Models--Testing (1)
• Airplanes--Wings, Swept-back (1)
• Charts, diagrams, etc (1)
• Wind tunnel testing (1) *

Author

• Fischetti, Thomas L. (1) *

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