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Elements of gas turbine propulsion / Jack D. Mattingly.

By: Mattingly, Jack DMaterial type: TextTextPublication details: New York : McGraw-Hill, 1996. ISBN: 0079121969Subject(s): aircraft engines | gas turbine enginesDDC classification: 621.433
Contents:
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.
Holdings
Item type Home library Call number Status Date due Barcode Item holds
Two Week Loan Two Week Loan College Lane Learning Resources Centre
Main Shelves 		629.134353 MAT (Browse shelf(Opens below)) Available 4403656379
Total holds: 0

Enhanced descriptions from Syndetics:

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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