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Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5

Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration

Flutter at very high speeds

Experimental investigation of the simulation of atmospheric entry of ballistic missiles

Published Year

• 1950-1959 (4) *

Subject

• Aerodynamic heating (4) *
• Charts, diagrams, etc (4)
• Aerodynamics, Supersonic (2)
• Body of revolution (2)
• Mathematics (2)
• Temperature measurements (2)
• Aerodynamics, Hypersonic (1)
• Aeroelasticity (1)
• Aerofoils (1)
• Ballistic missiles--Atmospheric entry (1)
• Cone--Aerodynamics (1)
• Cylinders--Aerodynamics (1)
• Engineering models (1)
• Flutter (Aerodynamics) (1)
• Heat--Transmission (1)
• Simulation (1)

Author

• Rumsey, Charles B. (2)
• Carson, James A. (1)
• Cunningham, Bernard E. (1)
• Hopko, Russell N. (1)
• Morgan, Homer G. (1)
• Neice, Stanford E. (1)
• Piland, Robert O. (1)
• Runyan, Harry L. (1)

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