TABLES OF SUPERSONIC FLOWS ABOUT CONE CYLINDERS. PART II. COMPLETE FLOWS

Abstract

Cylindrical coordinates and velocity components were tabulated at points of a characteristic net for a family of steady, nonviscous, axisymmetric, irrotational supersonic flows about cone cylinders with semi cone angles of 5k degrees (1 or = k < or = 10) and free stream Mach numbers 1.3, 1.5, 1.7, 2.0, 3. 0, 4.0, 5.0, and 7.0.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1950
Accession Number
AD0641349

Entities

People

  • J. H. Giese
  • R. F. Clippinger
  • W. C. Carter

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Axisymmetric
  • Bodies Of Revolution
  • Boundaries
  • Flow
  • Flow Fields
  • Free Stream
  • Grids
  • Mach Number
  • Maryland
  • Munitions
  • Shoulder
  • Supersonic Flow
  • Symmetry

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight