The article examines examples illustrating the semi-inverse method, devised by the author for solving the steady-state problem of hypersonic gas flow over a slender wing.

Original languageEnglish
Pages (from-to)47-52
Number of pages6
JournalFluid mechanics. Soviet research
Volume10
Issue number1
StatePublished - 1 Jan 1981

    Scopus subject areas

  • Engineering(all)

ID: 48961856