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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Abstract