Approach taken in design of components functioning as part of overall system, to maintain 70 F in passenger and crew areas at cruise altitude and ambient temperatures as low as -100 F and max of 75 F on hot day ground condition of 95 F DB and 78 F WB ambient; temperature control system comprising 3-port mix valve; distribution system, controlled air movement and space temperature, etc. (see also abstract in SAE -- J v 66 n 10 Oct 1958 p 32-4)
Air conditioned comfort on Douglas DC-8 jet transport
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1958 Aircraft
1958
13 pages
Aufsatz (Konferenz)
Englisch
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