Accession Number : AD0266924

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

Corporate Author : AVCO EVERETT RESEARCH LAB EVERETT MASS

Personal Author(s) : GEORGIEV,S. ; ROSE,P.H.

Report Date : DEC 1959

Pagination or Media Count : 1

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)

Descriptors :   *AUTORADIOGRAPHY, *HYPERSONIC FLOW, *HYPERSONIC WIND TUNNELS, *SIMULATION, AIR, CARBON, CONTAMINATION, ELECTRIC ARCS, ENTHALPY, FLUORENES, GUIDED MISSILE TRAJECTORIES, MATERIALS, PLASMAS(PHYSICS), PRODUCTION, TESTS, THERMODYNAMICS

Distribution Statement : APPROVED FOR PUBLIC RELEASE