EFFECTS OF CARBON CONTAMINATION OF AIR ON ABLATION ARC WIND TUNNEL TEST RESULTS

Abstract

AD-2 92410N3 AD-266 925LDiv. 9 U (TIPTP/MFA Army Ballistic Missile Agency, un sville, Al . CO PR IBLE FLOW TABLE k=1/24 SIMPLE GAS INJECTION WITH FORWARD VELOCITY EQUAL TO FREESTREAM VELOCITY y=1. 3 Nov 61, 89p. incl. tables (Rept. no. RA TR 1-18) U cl sified repor Notice: Only Government Agencies may request from STIA. Others re uest approval of Army Ballistic Mi sile Agency, Redston Aresenal, Ala. Attn: ORDAB-CL DESCRIPTORS: (*Compressible flow, * ables.) (Gases, Injection, Velocity, Ducts.) (Mach number, Specific hea .) (*Functions, Equa tions.) Functions of Mach numbers for a compressible perfect gas are tabulated The ratio of specific heats (k) is 1.24. The incre ent used in these tables is sufficiently small (0.001 Mach number) to eliminate time consuming interpola ion. The report covers simple gas injectio with forward velocity equal to freestream velocity in constant area ducts without friction and is one of a series of reports dealing with five simple types of one-dimensional flow. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1959
Accession Number
AD0266924

Entities

People

  • P.h. Rose
  • S. Georgiev

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ablation
  • Ballistic Missiles
  • Compressible Flow
  • Contamination
  • Flow
  • Friction
  • Governments
  • Mach Number
  • Motion
  • Physical Properties
  • Specific Heat
  • Wind Tunnel Tests
  • Wind Tunnels

Readers

  • Aerodynamics/Aeronautics.
  • Plasma Physics.
  • Snow Cover Descriptors for Reptiles and Their Illustrations.