Engineering Problems Associated with Supersonic Transport Aircraft: Choice of Materials for the Mach 2.2 SST, Results of Thermal Stresses, Choice of Glazing, Systems, Aircraft Heat Balance and Power Plant Design

Author： A.F.R.Ae.S. M.A. Taunton   A.M.I.Mech.E.  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.35, Iss.11, 1993-12, pp. : 326-331

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