NASA-TN-D-6283

A time-dependent method for calculating supersonic angle-of-attack flow about axisymmetric blunt bodies with sharp shoulders and smooth nonaxisymmetric blunt bodies

Note:

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Abstract:

Hypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based on time dependent finite difference theory and method of characteristics

Author(s):
R.W. Barnwell

Indexed under:

  • None

Details:

NASA-TN-D-6283
Format:
  • PDF (from scanned original)
Status:
  • Original, issued 01 Jan 1971
Previous Releases:
  • None available