"A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation" - Information and Links:

A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation - Info and Reading Options

"A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation" was published by National Aeronautics and Space Administration, Scientific and Technical Information Branch in 1981 - Washington, D.C, it has 37 pages and the language of the book is English.


“A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation” Metadata:

  • Title: ➤  A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
  • Author:
  • Language: English
  • Number of Pages: 37
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
  • Publish Date:
  • Publish Location: Washington, D.C

“A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation” Subjects and Themes:

Edition Specifications:

  • Pagination: 37 p. :

Edition Identifiers:

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