Inviscid aerodynamics of missiles with noncircular cross sections.

J. H. Huth

ResearchPublished 1952

A discussion of several methods which treat supersonic inviscid flow past ogive and cone cylinders with noncircular cross sections. In particular, the applications and limitations of relaxation and perturbation schemes are considered.

Document Details

  • Copyright: RAND Corporation
  • Availability: Web Only
  • Year: 1952
  • Pages: 21
  • Document Number: RM-992

Citation

Chicago Manual of Style

Huth, J. H., Inviscid aerodynamics of missiles with noncircular cross sections. Santa Monica, CA: RAND Corporation, 1952. https://www.rand.org/pubs/research_memoranda/RM992.html.
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