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

Author(s)

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

Bibliographic Information

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

Note

Title from cover

"Prepared by the Boeing Company for Langley Research Center"

Part 2: by E. D'Sylva

Details

• NCID: BA86425630
• LCCN: 70609156
• Country Code: us
• Title Language Code: eng
• Text Language Code: eng
• Place of Publication: Washington,Springfield
• Pages/Volumes: 2 v.
• Size: 27 cm
• Subject Headings:
  • FREE : Inviscid flow
  • FREE : Finite differences
  • FREE : Supersonic planes -- Design and construction
  • FREE : Computer programs
  • FREE : Flow charts
  • FREE : Flow equations.
• Parent Bibliography ID:
  • BA1162948X