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The design and testing of an axial-flow compressor having different blade profiles in each stage /

Bibliographic Details
Corporate Author: Aeronautical Research Council (Great Britain)
Other Authors: Carter, A. D. S.
Format: Book
Language:English
Published: London : Her Majesty's Stationery Office, 1960.
Series:Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3183.
Subjects:
Compressors > Aerodynamics.
Rotors > Dynamics.

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Call Number: TL526.G7 A4 no. 3183
 
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TL526.G7 A4 no. 3183 Available