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Gust-Tunnel Investigation of a Delta-Wing Model With the Leading Edge Swept Back 60 Degrees

Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region

Published Year

• 1950-1959 (2) *

Subject

• Aerodynamic load (1)
• Airplanes--Models--Testing (1)
• Airplanes--Models--Wings (1)
• Charts, diagrams, etc (1)
• Gust loads (1)
• Wind tunnel testing (1)

Author

• Pierce, Harold B. (2) *
• Reisert, Thomas D. (1)

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