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Gas turbine aero-thermodynamics : with special reference to aircraft propulsion / Sir Frank Whittle.

By: Whittle, Frank, 1907-1996.
Material type: materialTypeLabelBookSeries: Pergamon international library: Publisher: Oxford : Pergamon, 1981Description: xii, 261 p,[1]leaf of plates : ill, 1port ; 26 cm. + hbk.ISBN: 008026719X (cased); 0080267181 (v) (pbk) .Subject(s): Gas-turbines -- Dynamics | AerothermodynamicsDDC classification: 629.134353
Contents:
Section 1: Fundamentals -- Section 2: Flux density in isentropic compressible flow -- Section 3: Radial equilibrium in whirling isentropic compressible flow -- Section 4: A method of dealing with shock waves in air -- Section 5: Isentropic flow through nozzles -- Section 6: Representation of thermal cycles for perfect gases -- Section 7: Gas turbine cycle calculations using approximate methods -- Section 8: Turbo-gas generators -- Section 9: Mass flow rate in gas turbines -- Section 10: More on part load performance of gas generators -- Section 11: Gas turbines with recuperators -- Section 12: Turbo-compressors and turbines -- Section 13: Aircraft propulsion general -- Section 14: 'Ram' compression and intake design -- Section 15: Combustion -- Section 16: The 'straight' turbo jet -- Section 17: Effect on cycle calculations of more accurate methods -- Section 18: Calculation of maximum efficiency -- Section 19: 'Two spool' engines -- Section 20: Thrust boosting -- Section 21: Turbo fans -- Section 22: Effect of height and speed on performance -- Section 23: A super-thrust engine.
Holdings
Item type Current library Call number Copy number Status Date due Barcode Item holds
General Lending MTU Bishopstown Library Lending 629.134353 (Browse shelf(Opens below)) 1 Available 00009224
Total holds: 0

Section 1: Fundamentals -- Section 2: Flux density in isentropic compressible flow -- Section 3: Radial equilibrium in whirling isentropic compressible flow -- Section 4: A method of dealing with shock waves in air -- Section 5: Isentropic flow through nozzles -- Section 6: Representation of thermal cycles for perfect gases -- Section 7: Gas turbine cycle calculations using approximate methods -- Section 8: Turbo-gas generators -- Section 9: Mass flow rate in gas turbines -- Section 10: More on part load performance of gas generators -- Section 11: Gas turbines with recuperators -- Section 12: Turbo-compressors and turbines -- Section 13: Aircraft propulsion general -- Section 14: 'Ram' compression and intake design -- Section 15: Combustion -- Section 16: The 'straight' turbo jet -- Section 17: Effect on cycle calculations of more accurate methods -- Section 18: Calculation of maximum efficiency -- Section 19: 'Two spool' engines -- Section 20: Thrust boosting -- Section 21: Turbo fans -- Section 22: Effect of height and speed on performance -- Section 23: A super-thrust engine.

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