"Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts" - Information and Links:

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"Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts" was published by National Aerospace Laboratory in 1987 - Amsterdam, Netherlands and it has 45 pages.


“Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts” Metadata:

  • Title: ➤  Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts
  • Author:
  • Number of Pages: 45
  • Publisher: National Aerospace Laboratory
  • Publish Date:
  • Publish Location: Amsterdam, Netherlands

“Development of an advanced panel method for complex configurations in subsonic compressible flow; application to the computation of the potential flow through ducts” Subjects and Themes:

Edition Specifications:

  • Pagination: 45 p. :

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