A finite difference method for the solution of the transonic flow around harmonically oscillating wings /
by F. Edward Ehlers.

Description

Main Author

Ehlers, F. Edward.

Related Names

Langley Research Center.
Boeing Commercial Airplane Company.

Language(s)

English

Published

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

Subjects

Aerodynamics, Transonic > Aerodynamics, Transonic / Computer simulation.
Oscillating wings (Aerodynamics) > Oscillating wings (Aerodynamics) / Computer simulation.
Unsteady flow (Aerodynamics) > Unsteady flow (Aerodynamics) / Computer simulation.

Note

"Prepared by Boeing Commercial Aircraft Company ... for Langley Research Center."
Cover title.

Physical Description

iii, 79 p. : ill. ; 27 cm.

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