Concept of cooling passenger and crew compartments, as proposed by Boeing Co, utilizes air flowing outwardly through wall insulation to prevent aerodynamic heat from passing through wall; principle, called heat intercept system, was successfully tested on full scale aircraft body section; schematic of air conditioning and distribution system; aerodynamic heat flow into cabin can be reduced by 80% when 1.5 lb/hr/sq ft is allowed to pass through wall under conditions where outside skin temperature is 500 F; system is ideally suited for SST. (see also Heating and Vent Engr v 37 n 433 Aug 1963 p 61-6)


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    Title :

    Heat intercept cooling system for supersonic transport


    Additional title:

    SAE -- Paper


    Contributors:
    Newell, G.C. (author) / Evelyn, G.B. (author)

    Conference:

    SAE Meeting ; 1963 Aircraft



    Publication date :

    1963


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Heat Intercept Cooling System for the Supersonic Transport

    Evelyn, George B. / Newell, George C. | SAE Technical Papers | 1963



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