Elements of gas turbine propulsion /
Mattingly, Jack D.
Elements of gas turbine propulsion / Jack D. Mattingly ; with a foreword by Hans von Ohain. - New Delhi : TMH, 2013, c1996. - lxiii, 960 p. : - McGraw-Hill series in mechanical engineering McGraw-Hill series in aeronautical and aerospace engineering .
Includes bibliographical references (p. 945-948) and index.
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. 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.
9780070606289
95000897
Airplanes--Jet propulsion.
Jet engines.
Aircraft gas-turbines.
Jet engines
629.134353 / MAT
Elements of gas turbine propulsion / Jack D. Mattingly ; with a foreword by Hans von Ohain. - New Delhi : TMH, 2013, c1996. - lxiii, 960 p. : - McGraw-Hill series in mechanical engineering McGraw-Hill series in aeronautical and aerospace engineering .
Includes bibliographical references (p. 945-948) and index.
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. 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.
9780070606289
95000897
Airplanes--Jet propulsion.
Jet engines.
Aircraft gas-turbines.
Jet engines
629.134353 / MAT