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Numerical calculation of a three-dimensional laminar compressible boundary layer on profiled triangular wings with supersonic front edges

โœ Scribed by V. N. Vetlutskii; T. V. Poplavskaya


Publisher
SP MAIK Nauka/Interperiodica
Year
1994
Tongue
English
Weight
558 KB
Volume
34
Category
Article
ISSN
0021-8944

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