Aerospace Propulsion

Aerospace propulsion devices embody some of the most advanced technologies, ranging from materials, fluid control, and heat transfer and combustion. In order to maximize the performance, sophisticated testing and computer simulation tools are developed and used.

Aerospace Propulsion comprehensively covers the mechanics and thermal-fluid aspects of aerospace propulsion, starting from the fundamental principles, and covering applications to gas-turbine and space propulsion (rocket) systems. It presents modern analytical methods using MATLAB and other advanced software and includes essential elements of both gas-turbine and rocket propulsion systems. Gas turbine coverage includes thermodynamic analysis, turbine components, diffusers, compressors, turbines, nozzles, compressor-turbine matching, combustors and afterburners. Rocket coverage includes chemical rockets, electrical rockets, nuclear and solar sail.

Key features:

• Both gas-turbine and rocket propulsion covered in a single volume
• Presents modern analytical methods and examples
• Combines fundamentals and applications, including space applications
• Accompanied by a website containing MATLAB examples, problem sets and solutions

Aerospace Propulsion is a comprehensive textbook for senior undergraduate graduate and aerospace propulsion courses, and is also an excellent reference for researchers and practicing engineers working in this area.

Author: T. W. Lee
Publisher: Wiley
Published: 12/31/2013
Pages: 320
Binding Type: Hardcover
Weight: 1.45lbs
Size: 9.70h x 6.80w x 0.80d
ISBN: 9781118307984

About the Author

T.W. Lee, Arizona State University, USA

T.W. Lee is currently an Associate Professor in the Mechanical and Aerospace Engineering department at Arizona State University. He has been teaching an Aerospace Propulsion class for the last 15 years and is the author of two books. His research interests include combustion, thermal-fluids, and propulsion systems and current projects include hypersonic inlets and supersonic reactors.

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