Aeroplane and Commercial Aviation News, 87. kötet1954 |
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1 - 3 találat összesen 83 találatból.
22. oldal
... temperature of the main engine , the chief independent variable was the pressure ratio of the auxiliary compressor . The main turbine exhausts to the back - pressure of the auxiliary compressor ; therefore , if this back - pressure was ...
... temperature of the main engine , the chief independent variable was the pressure ratio of the auxiliary compressor . The main turbine exhausts to the back - pressure of the auxiliary compressor ; therefore , if this back - pressure was ...
25. oldal
... TEMPERATURE ROTOR NOZZLE GAS TEMPERATURE DESIGN ROTOR NOZZLE GAS TEMPERATURE 1500 ° K 1025 k THE AEROPLANE SPECIFIC FUEL CONSUMPTION LB / RHP - HR 2 2 له له 20 ROTOR TIP MACH No 7.008 50 60 1000K 1020 k K 70021 1400 ° K 100 Hunting ...
... TEMPERATURE ROTOR NOZZLE GAS TEMPERATURE DESIGN ROTOR NOZZLE GAS TEMPERATURE 1500 ° K 1025 k THE AEROPLANE SPECIFIC FUEL CONSUMPTION LB / RHP - HR 2 2 له له 20 ROTOR TIP MACH No 7.008 50 60 1000K 1020 k K 70021 1400 ° K 100 Hunting ...
8. oldal
... temperature ratio or the proportionate thrust boost rose , so the significance of the combustion Mach Number increased . At temperature ratios of the order of 1.5 : 1 , giving about 20 % thrust increase , it made little difference ...
... temperature ratio or the proportionate thrust boost rose , so the significance of the combustion Mach Number increased . At temperature ratios of the order of 1.5 : 1 , giving about 20 % thrust increase , it made little difference ...
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Wheelerhave been appointed by the Lord Chancellor | 19 |
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