Solution of problem of plane flow of gas past body in presence of circulation; solution obtained by CHAPLYGIN linear equations, assuming that K is constant. English translation from Prikladnaya Matematika i Mekhanika v 2 n 1 1947 p 105-18.
Subsonic gas flow past wing profile
Nat Advisory Committee Aeronautics -- Tech Memo
1950
29 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Calculation of a Subsonic or Transonic Wing Profile
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