Analysis of aerodynamic blade-loading-limit parameters for NACA 65-(C[sub zeta]₀A₁₀) 10 compressor-blade sections at low speeds /
By Melvyn Savage.

Description

Main Author

Savage, Melvyn.

Related Names

Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1955.

Subjects

Axial flow compressors > Axial flow compressors / Blades.
Axial flow compressors > Axial flow compressors / Aerodynamics.

Note

"April 25, 1955."

Physical Description

32 p. : ill. ; 27 cm.

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