CHARTS FOR CONICAL AND TWO-DIMENSIONAL OBLIQUE-SHOCK FLOW PARAMETERS IN HELIUM AT MACH NUMBERS FROM ABOUT 1 TO 100

Abstract

Charts are presented for the determination of certain flow properties in the flow field and on the surface of cones and wedges at Mach numbers from about 1 to 100 in a perfect gas with a ratio of specific heats of 5/3. In addition, a table of the isentropic subsonic flow parameters is included. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1961
Accession Number
AD0257852

Entities

People

  • Arthur Jr. Henderson
  • Dorothy O. Braswell

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Flow
  • Flow Fields
  • Mach Number
  • Physical Properties
  • Specific Heat
  • Subsonic Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.