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Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift

Published Year

• 1950-1959 (1)

Subject

• Aerodynamic load (1)
• Aerodynamics, Supersonic (1)
• Aerofoils--Testing (1)
• Charts, diagrams, etc (1)
• Drag (Aerodynamics) (1)
• Mach number (1) *
• Trailing edges (Aerodynamics) (1)

Author

• Katz, Ellis. (1)
• Morrow, John D. (1) *

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