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A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel

Factors affecting transition at supersonic speeds

Published Year

• 1950-1959 (2)

Subject

• Aerodynamics, Supersonic (2) *
• Airplanes--Fuselage (1)
• Boundary layer (1)
• Charts, diagrams, etc (1)
• Laminar flow (1)
• Supersonic planes (1)
• Surfaces (Physics) (1)
• Turbulence (1)

Author

• Sinclair, Archibald R. (2) *
• Czarnecki, K. R. (1)
• Hasel, Lowell E. (1)

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