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Span loadings due to wing twist at transonic and supersonic speeds

A tabulation of wind-tunnel pressure data at Mach numbers of 1.61 and 2.01 of five swept wings of the same plan form but different surface shapes

Published Year

• 1950-1959 (2)

Subject

• Airplanes--Wings, Swept-back (2) *
• Aerodynamic load (1)
• Aerodynamics, Supersonic (1)
• Aerodynamics, Transonic (1)
• Charts, diagrams, etc (1)

Author

• Grant, Frederick C. (2) *
• Mugler, John P. (1)

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