Sources of heated air were three exhaust-gas-to-air heat exchangers: one was located in each of the outboard nacelles and the third in the inboard nacelle. Tables show temperatures of heated circulating air and surfaces and capacity of heat exchangers in flights at 10,000 and 18,000 ft pressure altitude. Curves show the exhaust gas and circulating air-pressure drops for one of the exchangers based upon investigation in flight with exchanger installed in single-engine test airplane.
Development of Thermal Ice-Prevention Equipment for the B-17F Airplane
1943
50 pages
Report
Keine Angabe
Englisch
Development of thermal ice-prevention equipment for B-17F airplane
Engineering Index Backfile | 1943
|Development of thermal ice-prevention equipment for B-24D airplane
Engineering Index Backfile | 1943
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