Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small-disturbance equations

著者

• Gunness, R. C.
• Knight, C. J.
• D'Sylva, E
• Boeing Company
• Langley Research Center
• United States. National Aeronautics and Space Administration

書誌事項

Flow field analysis of aircraft configurations using a numerical solution to the three-dimensional unified supersonic/hypersonic small-disturbance equations

by R.C. Gunness, Jr., C.J. Knight, and E. D'Sylva

（NASA contractor report, NASA CR-1926-1927）

National Aeronautics and Space Administration , for sale by the National Technical Information Service, 1972

• Part 1
• Part 2

注記

Title from cover

"Prepared by the Boeing Company for Langley Research Center"

Part 2: by E. D'Sylva

詳細情報

• NII書誌ID(NCID): BA86425630
• LCCN: 70609156
• 出版国コード: us
• タイトル言語コード: eng
• 本文言語コード: eng
• 出版地: Washington,Springfield
• ページ数/冊数: 2 v.
• 大きさ: 27 cm
• 件名:
  • FREE : Inviscid flow
  • FREE : Finite differences
  • FREE : Supersonic planes -- Design and construction
  • FREE : Computer programs
  • FREE : Flow charts
  • FREE : Flow equations.
• 親書誌ID:
  • BA1162948X