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9 results returnedAn experimental investigation of the design variables for NACA submerged duct entrances
An inlet design concept to reduce flow distortion at angle of attack
Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet
Published Year
Subject
- Jet engines--Air intakes (9) *
- Charts, diagrams, etc (7)
- Air ducts (3)
- Aeronautics--Research (2)
- Diffusers (2)
- Drag (Aerodynamics) (2)
- Noses (Aircraft) (2)
- Pressure (2)
- Wind tunnel testing (2)
- Aerodynamic load (1)
- Aerodynamics, Supersonic (1)
- Air ducts--Aerodynamics (1)
- Air flow (1)
- Airplanes--Air ducts (1)
- Airplanes--Motors--Cowlings (1)
- Airplanes--Nacelles (1)
- Airplanes--Turbojet engines (1)
- Airplanes--Wings, Swept-back (1)
- Angle of attack (Aerodynamics) (1)
- Boundary layer (1)
- Boundary layer control (1)
- Compressors (1)
- Fighter planes (1)
- Fighter planes--Design and construction (1)
- Fighter planes--Research (1)
- Jet engines--Air intakes--Aerodynamics (1)
- Jet engines--Air intakes--Design and construction (1)
- Pressure--Measurement (1)
- Vibration (Aeronautics) (1)
Author
- Beheim, Milton A. (1)
- Campbell, Robert C. (1)
- Gault, Donald E. (1)
- Keith, Arvid L. (1)
- Mossman, Emmet A. (1)
- Nettles, J. Cary. (1)
- Pendley, Robert E. (1)
- Piercy, Thomas G. (1)
- Putland, Leonard W. (1)
- Randall, Lauros M., (1)
- Robinson, Harold L. (1)
- Schiff, Jack. (1)
- Schueller, Carl F. (1)
- Sears, R. I. (1)
- Stitt, Leonard E. (1)
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