Description: Design and R&D engineers and students will value the comprehensive coverage in this volume, which covers all aspects of aircraft propulsion systems. STANDARD PUBLISHER DISCLAIMER - Data and information appearing in this book are for informational purposes only. AIAA and the author are not responsible for any injury or damage resulting from use or reliance, nor do AIAA and the author warrant that use or reliance will be free from privately owned rights.
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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