Calculation of the pressure distribution on axisymmetric boattails including effects of viscous interactions and exhaust jets in subsonic flow /
by Josef Rom and Lawrence J. Bober.

Description

Main Author

Rom, Josef, 1932-

Related Names

Bober, Lawrence J.
Lewis Research Center.

Language(s)

English

Published

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

Subjects

Airplanes > Airplanes / Tail surfaces.
Turbulent boundary layer.
Jets > Jets / Fluid dynamics.
Viscous flow.
Aerodynamic load > Aerodynamic load / Measurement.

Note

Prepared at Lewis Research Center.
Cover title.

Physical Description

19 p. : ill. ; 27 cm.

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