Aerothermodynamics Of Gas Turbine And Rocket Propulsion PDF Download

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Aerothermodynamics of Gas Turbine and Rocket Propulsion

Aerothermodynamics of Gas Turbine and Rocket Propulsion
Author: Gordon C. Oates
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Total Pages: 480
Release: 1997
Genre: Science
ISBN:

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This seminal book on gas turbine technology has been a bestseller since it was first published. It now includes a comprehensive set of software programs that complement the text with problems and design analyses. Software topics included are atmosphere programs, quasi-one-dimensional flow programs (ideal constant-area heat interaction, adiabatic constant-area flow with friction, rocket nozzle performance, normal shock waves, oblique shock waves), gas turbine programs (engine cycle analysis and engine off-design performance), and rocket combustion programs (Tc and PC given, He and PC given, isentropic expansion).


Aerothermodynamics and Jet Propulsion

Aerothermodynamics and Jet Propulsion
Author: Paul G. A. Cizmas
Publisher: Cambridge University Press
Total Pages: 487
Release: 2021-12-02
Genre: Science
ISBN: 1108480756

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This robust introduction to aerothermodynamics uses example-based teaching to provide students with a solid theoretical foundation linked to real-world engineering scenarios.


Gas Turbine Aero-Thermodynamics

Gas Turbine Aero-Thermodynamics
Author: F. Whittle
Publisher: Elsevier
Total Pages: 276
Release: 2013-10-22
Genre: Technology & Engineering
ISBN: 1483293211

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For the first time simplified methods of dealing with gas turbine thermal cycles, and further theoretical innovations, have been embodied into a concise textbook. All the major aspects of the subject are covered in a comprehensive and lucid manner. Examples are included for greater clarity


Elements of Propulsion

Elements of Propulsion
Author: Jack D. Mattingly
Publisher: American Institute of Aeronautics and Astronautics Incorporated
Total Pages: 0
Release: 2016
Genre: Aircraft gas-turbines
ISBN: 9781624103711

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Elements of Propulsion: Gas Turbines and Rockets, Second Edition provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. Textbook coverage has been revised and expanded, including a new chapter on compressible flow. Design concepts are introduced early and integrated throughout. Written with extensive student input, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles.