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

By: Mattingly, Jack D Material type: Text

TextSeries: McGraw-Hill series in mechanical engineering: ; McGraw-Hill series in aeronautical and aerospace engineering: Publisher: New York : McGraw-Hill, c1996Description: lxiii, 960 p. : ill. ; 25 cm.+ 1 computer disk (3 1/2 in.)ISBN: 0071145214Subject(s): Airplanes -- Jet propulsion | Jet engines | Aircraft gas-turbines | Jet enginesDDC classification: 629.134353 LOC classification: TL709 | .M38 1996Online resources: Publisher description | Table of contents

Contents:

Introduction -- Thermodynamics Review -- Compressible Flow -- Aircraft Gas Turbine Engine -- Parametric Cycle Analysis of Ideal Engines -- Component Performance -- Parametric Cycle Analysis of Real Engines -- Engine Performance Analysis -- Turbomachinery -- 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.

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Item type	Current location	Home library	Shelving location	Call number	Status	Date due	Barcode	Item holds
Book	School of Mechanical & Manufacturing Engineering (SMME)	School of Mechanical & Manufacturing Engineering (SMME)	Aerospace Engineering	629.134353 MAT (Browse shelf)	Available		SMME-1554

Total holds: 0

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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.

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