Oates G. — Aircraft Propulsion Systems Technology and Design
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Название: Aircraft Propulsion Systems Technology and Design
Автор: Oates G.
Аннотация:
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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О проекте