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Accession Number:
AD0760015
Title:
Thoughts and Afterthoughts About Shock Computations.
Descriptive Note:
Research rept.,
Corporate Author:
POLYTECHNIC INST OF BROOKLYN FARMINGDALE N Y DEPT OF AEROSPACE ENGINEERING AND APPLIED MECHANICS
Report Date:
1972-12-01
Pagination or Media Count:
89.0
Abstract:
Typical one-dimensional, unsteady flow problems are considered to support shock-fitting concepts as the best way to handle shocked flows. Shock-captureing experiments are discussed their results are concluded to be unsatisfactory. Various methods to predict the formation of a shock are suggested. Four shock-fitting methods are discussed, two of them considering the shock as a boundary between regions of continuous flow and two letting the shock move between mesh points. Author
Distribution Statement:
APPROVED FOR PUBLIC RELEASE