000 | 01600nam a22004577a 4500 | ||
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001 | NM003252 | ||
003 | AR-HaUTN | ||
007 | ta | ||
008 | 03020sc. 1 ||||||||||||||000 | spa|| | ||
005 | 20240930172308.0 | ||
020 | _a080267181 | ||
040 | _aarhautn | ||
100 |
_aWhittle, Frank _98004 |
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245 |
_aGas turbine aero-thermodynamics _bwith special reference to aircraft propulsion _cFrank Whittle |
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260 |
_aOxford _bPergamon |
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300 | _axii, 261 p. | ||
505 | _tFundamentals | ||
505 | _tFlux density in isentropic compressible flow | ||
505 | _tRadial equilibrium in whirling isentropic compressible flow | ||
505 | _tA method of dealing with shock waves in air | ||
505 | _tIsentropic flow through nozzles | ||
505 | _tRepresentation of thermal cycles for perfect gases | ||
505 | _tGas turbine cycle calculations using approximate methods | ||
505 | _tTurbo-gas generators | ||
505 | _tMass flow rate in gas turbines | ||
505 | _tMore on part load performance of gas generators | ||
505 | _tGas turbines with recuperators | ||
505 | _tTurbo-compressors and turbines | ||
505 | _tAircraft propulsion general | ||
505 | _t"Ram" compression and intake design | ||
505 | _tCombustion | ||
505 | _tThe "straigth" turbo jet | ||
505 | _tEffect on cycle calculations of more accurate methods | ||
505 | _tCalculation of maximum efficiency | ||
505 | _t"Two spool" engines | ||
505 | _tThrust boosting | ||
505 | _tTurbo fans | ||
505 | _tEffect of height and speed on performance | ||
505 | _tA super-thrust engine | ||
942 | _cBK | ||
999 |
_c3252 _d3252 |