Application of shock tubes to transonic airfoil testing at high Reynolds numbers /
William J. Cook ... [et al.], Iowa State University.

Description

Corporate Author

United States. National Aeronautics and Space Administration.

Related Names

Cook, William John, 1929-, joint author.
Iowa State University.

Language(s)

English

Published

[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; 1978.

Subjects

Aerofoils.
Shock tubes.

Note

Nov. 1978.

Physical Description

vi, 63 p. : ill. ; 27 cm.

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