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Analysis of penetration and mixing of gas jets in supersonic cross flowThe JETPEN analysis for gas jets in a supersonic cross flow developed earlier at APL/JHU has been extended in several important ways. First, the treatment of cases with injection at angles other than 90 deg has been redone. Next, the second of the three regions formerly treated has been eliminated. Third, the region downstream of the Mach disk for underexpanded cases has been reformulated such that turbulent entrainment of main stream fluid into the plume is modeled, and the equations of motion are solved marching downstream. These changes now permit prediction of the variation in composition, mixing area growth and all other flow variables along the plume. The analysis has been verified by comparison of predictions and experiment over a wide range of conditions. The result is an analysis capable of reliable predictions of the major flowfield variables that can be run on a PC.
Document ID
19930038334
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Billig, F. S.
(Johns Hopkins Univ. Laurel, MD, United States)
Schetz, J. A.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, United States)
Date Acquired
August 16, 2013
Publication Date
December 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 92-5061
Meeting Information
Meeting: AIAA, International Aerospace Planes Conference
Location: Orlando, FL
Country: United States
Start Date: December 1, 1992
End Date: December 4, 1992
Sponsors: AIAA
Accession Number
93A22331
Distribution Limits
Public
Copyright
Other

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