Aerothermodynamics of Gas Turbine and Rocket Propulsion – Gordon C. Oates – 3rd Edition

Description

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).

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  • Chapter 1. Thermodynamics and Quasi-One-Dimensional Fluid Flows
    Chapter 2. Chemical Rockets
    Chapter 3. Nonchemical Rockets
    Chapter 4. Ideal Cycle Analysis
    Chapter 5. Component Performance
    Chapter 6. Nonideal Cycle Analysis
    Chapter 7. Engine Off-Design Performance
    Chapter 8. Elementary Theory of Blade Aerodynamics
    Chapter 9. Throughflow Theory
    Chapter 10. Cascade Flows
  • Citation
    • Full Title: Aerothermodynamics of Gas Turbine and Rocket Propulsion
    • Author/s:
    • ISBN-10: 1563472414
    • ISBN-13: 9781563472411
    • Edition: 3rd Edition
    • Publication date: 1997
    • Topic: Engineering
    • Subtopic: Mechanical Engineering
    • File Type: eBook
    • Idioma: English

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459 pag.
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