Research on rotating stall in axial flow compressors.
Part I. On lift hysteresis at maximum lift including effect of camber /
R.A. Hartunian.

Description

Main Author

Hartunian, R. A.

Related Names

Wright Air Development Center
United States. Air Force.

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959.

Subjects

Hysteresis.
Camber (Aerofoils)
Lift (Aerodynamics)

Note

"Cornell Aeronautical Laboratory, Inc., Buffalo, New York."
"Project No. 3066, Task No. 70181."
"Aeronautical Research Laboratory."
"January 1959."
"ASTIA Document No. AD 216301"

Physical Description

vii, 25 pages illustrations, tables ; 28 cm

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