Attempt is made to find most favorable speed-altitude schedule for transport or bomber, with minimum shock-wave noise as prime consideration; propagation of shock waves for case of homogeneous atmosphere and also for normal atmosphere exhibiting temperature and wind gradients, recent experimental results and available theory concerning "sonic boom" given.
Sonic boom -- Limitations on supersonic aircraft operations
Aero/Space Eng
Aerospace Engineering ; 19 , n 7
1960
2 pages
Article (Journal)
English
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