Aeroplane and Commercial Aviation News, 89. kötet1955 |
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17. oldal
... temperature whereas for a turboprop both power and specific fuel consumption continue to improve with rising combustion temperature . For the turboprop at 400 m.p.h. and 36,000 ft . , range continues to improve with increasing flame ...
... temperature whereas for a turboprop both power and specific fuel consumption continue to improve with rising combustion temperature . For the turboprop at 400 m.p.h. and 36,000 ft . , range continues to improve with increasing flame ...
18. oldal
... temperature of 243 ° C. at sea - level and a temperature of 115 C. in the stratosphere . At a speed of Mach 3 these figures become 535 ° C. and 335 ° C. respectively . Such temperatures dictate both the performance and metallurgy of an ...
... temperature of 243 ° C. at sea - level and a temperature of 115 C. in the stratosphere . At a speed of Mach 3 these figures become 535 ° C. and 335 ° C. respectively . Such temperatures dictate both the performance and metallurgy of an ...
9. oldal
... temperature on take - off distance was small . For instance , at an aerodrome at an altitude of 2,500 ft . and with a temperature of 25 ° C. the minimum field length was 5,850 ft . at a gross weight of 60,000 lb. The use of water ...
... temperature on take - off distance was small . For instance , at an aerodrome at an altitude of 2,500 ft . and with a temperature of 25 ° C. the minimum field length was 5,850 ft . at a gross weight of 60,000 lb. The use of water ...
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