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Ability to control the sonic boom level by means of aerodynamic surfaces
Author(s) -
A. V. Potapkin,
D. Yu. Moskvichev
Publication year - 2017
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.5007614
Subject(s) - sonic boom , aerodynamics , mach number , supersonic speed , mechanics , shock wave , acoustics , physics , wind tunnel , shock (circulatory) , supersonic wind tunnel , aerospace engineering , aerodynamic force , engineering , medicine

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