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)
Heat intercept cooling system for supersonic transport
SAE -- Paper
SAE Meeting ; 1963 Aircraft
1963
8 pages
Conference paper
English
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Heat Intercept Cooling System for the Supersonic Transport
SAE Technical Papers | 1963
|NTRS | 1963
TIBKAT | 2023
|Online Contents | 2011
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