Aerodynamic aspects of engine air intake for Anglo-French Concorde aircraft; mounted under wing of Concorde, inlet is divided to provide independent supplies of air to pair of engines, specific arrangement that introduces particular problems in allowing for wing flow-field and avoiding interaction between twin inlets; factors considered in choice of compression system and intake geometry; aerodynamic and other development tests required to make appropriate decisions are described showing suitability of basic geometry in association with other components of propulsion system for SST operation. (13357)
Design and development of air intake for supersonic transport aircraft
J Aircraft
Journal of Aircraft ; 5 , n 6
1968
9 pages
Article (Journal)
English
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