Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages
By: Ronald J. Steinke.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2597.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1987
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Compressors.; Axial flow compressors.
Other titles: Design of 9.271 pressure ratio five stage core compressor and overall performance for first three stages.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche.