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Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles

Internal performance characteristics of short convergent-divergent exhaust nozzles designed by the method of characteristics

Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air

Effects on adjacent surfaces from the firing of rocket jets

Published Year

• 1950-1959 (4) *

Subject

• Charts, diagrams, etc (4)
• Waste gases (4) *
• Air flow (2)
• Pressure (2)
• Aerodynamics, Supersonic (1)
• Boundary layer (1)
• Ejector pumps (1)
• Gas flow (1)
• Gas-turbines (1)
• Guided missiles (1)
• Nozzles (1)
• Nozzles--Design and construction (1)
• Nozzles--Performance (1)
• Rocket engines (1)
• Rockets (Aeronautics) (1)

Author

• Beale, William T. (1)
• Bressette, Walter E. (1)
• Connors, James F. (1)
• Cubbison, Robert W. (1)
• Hearth, Donald P. (1)
• Krull, H. George. (1)
• Leiss, Abraham. (1)
• Meyer, Rudolph C. (1)

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