Date of Award

12-1994

Document Type

Dissertation

Degree Name

Doctor of Philosophy (PhD)

First Advisor

William C. Elrod, PhD

Abstract

The effects of varying the exit pressure of a supersonic helium jet exhausting coaxially with two parallel supersonic air streams into a constant area duct were investigated. The method used to evaluate the mass entrainment rate was to measure helium molar concentration profiles and mass flux across the duct using a binary gas probe then calculate the mass entrainment into the helium jet. In order to conduct this study a novel binary gas probe was developed which allowed helium concentration and mass flux data to be obtained during continuous traverses across the supersonic flowfield. High exit pressure ratio (EPR) led to improved overall mixing compared to the baseline case with an EPR near unity. The high EPR caused low mass entrainment along the jet shear layers due to high convective Mach numbers and velocity ratios, but the high EPR caused oblique shocks to form which reflected off the duct walls and intersected with the helium jet several times causing significant mass entrainment due to numerous shock-shear layer interactions (SSLIs). A correlation between the vorticity generated during a SSLI and the mass entrainment into the jet was developed.

AFIT Designator

AFIT-DS-AA-94-6

DTIC Accession Number

ADA290859

Comments

Presented to the Faculty of the School of Engineering of the Air Force Institute of Technology.

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