| 000 | 01600mm a2200457a 44500 | ||
|---|---|---|---|
| 001 | NM003252 | ||
| 003 | AR-HaUTN | ||
| 007 | ta | ||
| 008 | 03020sc. 1 ||||||||||||||000 | spa|| | ||
| 005 | 20240912185435.0 | ||
| 020 | _a080267181 | ||
| 040 | _aarhautn | ||
| 100 |
_aWhittle, Frank _98004 |
||
| 245 |
_aGas turbine aero-thermodynamics _bwith special reference to aircraft propulsion _cFrank Whittle |
||
| 260 |
_aOxford _bPergamon |
||
| 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 |
||