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Analytical and experimental investigation of inlet-engine matching for turbojet-powered aircraft at Mach numbers up to 2.0

An inlet design concept to reduce flow distortion at angle of attack

Published Year

• 1950-1959 (2) *

Subject

• Air ducts (1)
• Air flow (1)
• Charts, diagrams, etc (1)
• Diffusers (1)
• Jet engines--Air intakes (1)
• Pressure--Measurement (1)

Author

• Schueller, Carl F. (2) *
• Stitt, Leonard E. (1)

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