Open AccessThe effect of the afterbody of the supersonic civil aircraft model on the terminal shock wave forming in the sonic boom wave profile
Author(s) -
В. Ф. Волков
Publication year - 2021
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/5.0054106
Subject(s) - sonic boom , supersonic speed , shock wave , shock (circulatory) , aerospace engineering , propulsion , closing (real estate) , acoustics , terminal (telecommunication) , boom , mechanics , physics , engineering , telecommunications , medicine , environmental engineering , political science , law
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