Theoretical Analysis of the Flow Field Over a Family of Ogive Bodies. Supplement.

Abstract

Local body surface pressure coefficients and Mach numbers are presented for tangent ogive bodies at Mach numbers from 2 to 4.5 and at 0 and 2 deg angle-of-attack. These data were obtained using the US Army Missile Research and Development Command three-dimensional method of characteristics computer code. This volume is intended to supplement MIRADCOM Technical Report TD-CR-77-5, published August 1977. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jan 12, 1979
Accession Number
ADA065416

Entities

People

  • B. Z. Jenkins
  • R. L. Richardson

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Bodies
  • Bodies Of Revolution
  • California
  • Corporations
  • Engineering
  • Flow
  • Flow Fields
  • Free Stream
  • Jet Propulsion
  • Mach Number
  • Mechanical Engineering
  • Method Of Characteristics
  • Ordnance Laboratories
  • Physics Laboratories
  • Three Dimensional
  • United States

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Structural Dynamics.
  • Technical Research and Report Writing.