Effect of steady-state temperature distortion on inlet flow to a high-bypass-ratio turbofan engine
By: Ronald H. Soeder and Charles M. Mehalic and Kevin Stancik
Contributors: Mehalic, Charles M; Stancik, Kevin; Lewis Research Center
Series: NASA technical memorandum -- 86896
Publisher: Lewis Research Center
Published: 1985
Place of publication: Cleveland, Ohio
Language: eng
Format: Microform
Subjects: Turbines
Notes: "January 1985."

Bibliography: p. 10-11

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1985. 1 microfiche ; 11 x 15 cm