Accession Number : AD0871755

Title :   An Oil Flow Study of a Sonic Reaction Jet Ejecting from a Body of Revolution into a Free Stream of Mach Number Range 1.75 to 4.5.

Descriptive Note : Technical rept.,

Corporate Author : ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL AER OBALLISTICS DIRECTORATE

Personal Author(s) : Street, Troy A.

Report Date : 21 APR 1970

Pagination or Media Count : 355

Abstract : An oil flow test was conducted to obtain flow patterns in the vicinity of a transverse sonic jet ejecting from a body of revolution into an oncoming supersonic flow of M = 1.75, 2.0, 3.0, 4.0, and 4.5. The angle of attack was plus or minus 10 degrees with jet total-to-free stream static pressure ratios up to 100. The jet was oriented to various angular positions at several longitudinal body locations. (Author)

Descriptors :   *CONTROL JETS), (*GUIDED MISSILES, SUPERSONIC CHARACTERISTICS, BODIES OF REVOLUTION, EJECTION, FLOW VISUALIZATION, ANGLE OF ATTACK, PRESSURE.

Subject Categories : Guided Missiles
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE