The effect of compressor seventh-stage bleed air extraction on performance of the F100-PW-220 afterburning turbofan engine
By: Alison B. Evans.
Contributors: Dryden Flight Research Facility.
Series: NASA contractor report -- 179447.; NASA contractor report -- NASA CR-179447.
Publisher: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
Published: 1991
Place of publication: Edwards, Calif
Language: eng
Format: Microform
Subjects: Airplanes -- United States -- Motors -- Thrust.
Other titles: Effect of compressor seventh stage bleed air extraction on performance of the F100-PW-220 afterburning turbofan engine.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.] : National Aeronautics and Space Administration, [1991] 1 microfiche.