Use of potential flow theory to evaluate subsonic inlet data from a simulator-powered nacelle at cruise conditions /
Lawrence J. Bober.

Description

Main Author

Bober, Lawrence J.

Related Names

Lewis Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1974.

Subjects

Drag (Aerodynamics)
Aerodynamic load.
Airplanes > Airplanes / Nacelles.
Airplanes > Airplanes / Turbofan engines.
Air ducts > Air ducts / Aerodynamics > Air ducts / Aerodynamics / Mathematical models.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Air intakes > Airplanes / Turbojet engines / Air intakes / Mathematical models.

Note

Prepared at Lewis Research Center.
Cover title.

Physical Description

24 p. : ill. ; 27 cm.

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