Elements of gas turbine propulsion
Author(s)
Bibliographic Information
Elements of gas turbine propulsion
（McGraw-Hill series in mechanical engineering）（McGraw-Hill series in aeronautical and aerospace engineering）
McGraw-Hill, c1996
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Note
Includes bibliographical references (p. 945-948) and index
Description and Table of Contents
Description
This text provides an introduction to the fundamentals of gas turbine engines and jet propulsion for aerospace or mechanical engineers. The book contains sufficient material for two sequential courses i propulsion (advanced fluid dynamics) an introductory course in jet propulsion and a gas turbine engine components course. The text is divided into four parts introduction to aircraft propulsion; basic concepts and one-dimensional/gas dynamics; analysis and performance of air breathing propulsion systems; and analysis and design of gas turbine engine components.
Table of Contents
1 Introduction2 Thermodynamics Review3 Compressible Flow4 Aircraft Gas Turbine Engine5 Parametric Cycle Analysis of Ideal Engines6 Component Performance7 Parametric Cycle Analysis of Real Engines8 Engine Performance Analysis9 Turbomachinery10 Inlets, Nozzles and Combustion SystemsAppendixesA U.S. Standard Atmosphere, 1976B Gas Turbine Engine DataC Rocket Engine DataD Air and (CH2)n Properties at Low PressureE Compressible Flow FunctionsF Normal Shock FunctionsG Two-Dimensional Oblique Flow FunctionsH Rayleigh Line Flow FunctionsI Fanno Line Flow FunctionsJ Turbomachinery Stresses and MaterialsK About the Software
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