Supersonic Flow about Right Circular Cones at Zero Yaw in Air at Thermodynamic Equilibrium. Part 3. Tables of Data, Continued

Abstract

This material is a continuation of Part II and presents the cone flow properties of air in chemical equilibrium for altitudes from 100,000 to 200,000 feet at cone angles of 2.5 to 50 degrees, and various Mach numbers from 3.0 to 40.0. Part II presents the cone properties for altitudes from sea level to 80,000 feet. Part I presents an analysis and correlation of this data. The Table of Symbols has been reproduced in this report for the convenience of the reader.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1964
Accession Number
AD0451469

Entities

People

  • Henry Hudgins

Organizations

  • Picatinny Arsenal

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Altitude
  • California
  • Cartesian Coordinates
  • Chemical Equilibrium
  • Engineering
  • Flow
  • Mach Number
  • Munitions
  • New Mexico
  • Nuclear Engineering
  • Ordnance Laboratories
  • Plastic Explosives
  • Sea Level
  • Supersonic Flow
  • Three Dimensional

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics
  • Fluid Dynamics.

Technology Areas

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