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Tests of a small-scale NACA submerged inlet at transonic Mach numbers

Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8

Preliminary attempts at isothermal compression of a supersonic air stream

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

Flight determination of drag and pressure recovery of two scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8

Effects on adjacent surfaces from the firing of rocket jets

Published Year

• 1950-1959 (6)

Subject

• Charts, diagrams, etc (6)
• Pressure (6) *
• Air flow (2)
• Drag (Aerodynamics) (2)
• Jet engines--Air intakes (2)
• Waste gases (2)
• Aerodynamics, Supersonic (1)
• Aeronautics--Research (1)
• Air ducts (1)
• Airplanes--Fuselage (1)
• Aspect ratio (Aerofoils) (1)
• Boundary layer control (1)
• Diffusers (1)
• Gas flow (1)
• Gas-turbines (1)
• Guided missiles (1)
• Mach number (1)
• Noses (Aircraft) (1)
• Nozzles--Performance (1)
• Rocket engines (1)
• Rockets (Aeronautics) (1)

Author

• Beale, William T. (1)
• Bressette, Walter E. (1)
• Krull, H. George. (1)
• Leiss, Abraham. (1)
• Perchonok, E. (1)
• Putland, Leonard W. (1)
• Rathert, George A., (1)
• Rolls, L. Stewart. (1)
• Sears, R. I. (1)
• Wilcox, F. (1)

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