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 Report

Corporate Author:

ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL REDSTONE ARSENAL

Personal Author(s):

• Street,Troy A.

Report Date:

1970-04-21

Pagination or Media Count:

345.0

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.

Descriptors:

• CONTROL JETS
• GUIDED MISSILES
• SUPERSONIC CHARACTERISTICS
• BODIES OF REVOLUTION
• EJECTION
• FLOW VISUALIZATION
• ANGLE OF ATTACK
• PRESSURE

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE