Aircraft propulsion systems technology and design /

A comprehensive coverage of the key physical concepts that govern gas turbine propulsion systems. Topics include combustion technology, engine/airplane performance matching, inlets and inlet/engine integration, variable convergent/divergent nozzle aerodynamics, and more

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Bibliographic Details
Other Authors: Oates, Gordon C
Format: Book
Language:English
Published: Washington, DC : American Institute of Aeronautics and Astronautics , c1989
Washington, DC : American Institute of Aeronautics and Astronautics, c1989
Washington, DC : [1989]
Series:AIAA education series
AIAA education series
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Stanford University

Holdings details from Stanford University
Call Number: ISIL:US-CST
TL709 .A44 1989

Massachusetts Institute of Technology

Holdings details from Massachusetts Institute of Technology
Call Number: TL709.A44 1989

Duke University

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Call Number: TL709 .A44 1989

Cornell University

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Call Number: TL709 .A29 1989

Princeton University

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Call Number: TL709 .A44 1989

University of Pennsylvania

Holdings details from University of Pennsylvania
Call Number: TL709 .A44 1989