Aerodynamic and structural problems encountered in construction of supersonic aircraft; consequences of high speed effects on aircraft systems reviewed; operating costs of both Mach 2+ and Mach 3 transport are discussed in particular; it is concluded that while Mach 2 poses many new and complex problems, advance in techniques required can be regarded as typical step forward in history of aviation; Mach 3 however, demands novel departures from existing experience in almost all features of engine.
Supersonic transport aircraft
Ingenieur
Ingenieur ; 74 , n 15
1962
Article (Journal)
English
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