Effect of combined pressure and temperature distortion orientation on high-bypass-ratio turbofan engine stability
By: Ronald H. Soeder and Charles M. Mehalic
Contributors: Mehalic, Charles M; United States. National Aeronautics and Space Administration
Series: NASA technical memorandum -- 83771
Publisher: National Aeronautics and Space Administration
Published: 1984
Place of publication: [Washington, D.C.]
Language: eng
Format: Microform
Subjects: Airplanes -- Turbofan engines
Notes: Cover title

Distributed to depository libraries in microfiche

"October 1984."

STAR category 07

Bibliography: p. 16-17

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1984. 1 microfiche ; 11 x 15 cm