Elements of gas turbine propulsion / Jack D. Mattingly ; with a foreword by Hans von Ohain.

Includes bibliographical references (p. 945-948) and index.

1. Introduction -- 2. Thermodynamics Review -- 3. Compressible Flow -- 4. Aircraft Gas Turbine Engine -- 5. Parametric Cycle Analysis of Ideal Engines -- 6. Component Performance -- 7. Parametric Cycle Analysis of Real Engines -- 8. Engine Performance Analysis -- 9. Turbomachinery -- 10. Inlets, Nozzles, and Combustion Systems -- App. A. U.S. Standard Atmosphere, 1976 -- App. B. Gas Turbine Engine Data -- App. C. Data for Some Liquid Propellant Rocket Engines -- App. D. Air and (CH[subscript 2]), Properties at Low Pressure -- App. E. Compressible Flow Functions ([gamma] = 1.4, 1.33, and 1.3) -- App. F. Normal Shock Functions ([gamma] = 1.4) -- App. G. Two-Dimensional Oblique Shock Functions ([gamma] = 1.4) -- App. H. Rayleigh Line Flow Functions ([gamma] = 1.4) -- App. I. Fanno Line Flow Functions ([gamma] = 1.4) -- App. J. Turbomachinery Stresses and Materials -- App. K. About the Software.