Experimental investigation of advanced concepts to increase turbine blade loading :
V. Performance evaluation of jet-flap rotor blade /
by H.G. Lueders.

Description

Main Author

Lueders, H. G.

Related Names

United States. National Aeronautics and Space Administration.
Lewis Research Center.
General Motors Corporation.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration, 1970.

Subjects

Turbines > Turbines / Blades > Turbines / Blades / Testing.
Vortex generators > Vortex generators / Testing.

Note

Prepared by General Motors for Lewis Research Center.
N70-25826.

Physical Description

v, 69 p. : ill. ; 27 cm.

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