Numerical solution of the problem of unsteady supersonic flow around the front part of the wings with a detached shock wave
G.P. VoskresenskyVolume:
19
Année:
1979
Langue:
english
Pages:
19
DOI:
10.1016/0045-7825(79)90078-1
Fichier:
PDF, 1.31 MB
english, 1979