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 Soc Automotive Engrs -- Paper n 87A for meeting Sept 29-Oct 4 1958 13 p)
Air conditioned comfort on Douglas DC-8 jet transport
SAE -- J
Society of Automotive Engineers -- Journal ; 66 , n 10
1958
3 pages
Article (Journal)
English
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Air conditioned comfort on Douglas DC-8 jet transport
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