Comparisons of two-dimensional shock-expansion theory with experimental aerodynamic data for delta-planform wings at high supersonic speeds /
by Lloyd S. Jernell.

Description

Main Author

Jernell, Lloyd S.

Related Names

Langley Research Center.

Language(s)

English

Published

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

Subjects

Aerodynamics, Hypersonic.
Aerodynamics, Supersonic.
Aerofoils.
Airplanes > Airplanes / Wings, Triangular.

Note

Prepared at Langley Research Center.
Cover title.

Physical Description

36 p. : ill. ; 27 cm.

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