Aeroplane and Commercial Aviation News, 85. kötet1953 |
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25. oldal
... thrust output . Again with reheat , there is a small percentage loss in thrust , when reheat is inoperative , because of pressure losses from the obstructions in the tail pipe . If the rocket is jettisoned there is no permanent aircraft ...
... thrust output . Again with reheat , there is a small percentage loss in thrust , when reheat is inoperative , because of pressure losses from the obstructions in the tail pipe . If the rocket is jettisoned there is no permanent aircraft ...
31. oldal
... thrust augmentation of engine wake , chief among which is the necessity for controlling the area of the exit nozzle of the tailpipe . This area variation of the nozzle is necessary in order to provide the desired turbine temperature and ...
... thrust augmentation of engine wake , chief among which is the necessity for controlling the area of the exit nozzle of the tailpipe . This area variation of the nozzle is necessary in order to provide the desired turbine temperature and ...
34. oldal
1.6 ON NIMONIC ALLOYS 26 / HT / 61 THE AEROPLANE. THE AEROPLANE THRUST THRUST AT M - 1.5 1.0 BASIC TURBO - JET .75 TURBO - JET WITH .5 - AFTERBURNER RAM JET LO 1.5 FLIGHT MACH NUMBER Fig . 1 Typical engine thrust characteristics ...
1.6 ON NIMONIC ALLOYS 26 / HT / 61 THE AEROPLANE. THE AEROPLANE THRUST THRUST AT M - 1.5 1.0 BASIC TURBO - JET .75 TURBO - JET WITH .5 - AFTERBURNER RAM JET LO 1.5 FLIGHT MACH NUMBER Fig . 1 Typical engine thrust characteristics ...
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