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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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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//IF NOT LOGGED IN - FORCE LOGIN ?> //ELSE THEY ARE LOGGED IN PROCEED WITH THE OPEN URL CODE:?>Stanford University
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ISIL:US-CST TL709 .A44 1989 |
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Massachusetts Institute of Technology
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TL709.A44 1989 |
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Duke University
Call Number: |
TL709 .A44 1989 |
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Cornell University
Call Number: |
TL709 .A29 1989 |
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Princeton University
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TL709 .A44 1989 |
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University of Pennsylvania
Call Number: |
TL709 .A44 1989 |
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