Comparison of three methods for calculation of helicopter rotor blade loading and stresses due to stall /
by Wayne Johnson.

Description

Main Author

Johnson, Wayne, 1946-

Related Names

U.S. Army Air Mobility Research and Development Laboratory.
Ames Research Center.

Language(s)

English

Published

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

Subjects

Aerodynamic load.
Stalling (Aerodynamics)
Rotors (Helicopters) > Rotors (Helicopters) / Aerodynamics.

Note

Prepared at Ames Research Center and the U.S. Army Air Mobility R&D Laboratory.
Cover title.

Physical Description

iv, 21 p. : ill. ; 27 cm.

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