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Accession Number:
AD0672282
Title:
COMPUTATION OF AXIAL-SYMMETRIC TRANSONIC SWIRL FLOWS BY THE UNSTEADY FLOW APPROACH. APPENDIX: CHECK OF THE ACCURACY OF THE RESULTS,
Descriptive Note:
Corporate Author:
AEROSPACE RESEARCH LABS WRIGHT-PATTERSON AFB OHIO
Report Date:
1968-04-01
Pagination or Media Count:
82.0
Abstract:
Steady flows through a Laval nozzle with and without swirl are computed as the long time limit of unsteady flow fields by means of a three dimensional method of characteristics. In an appendix the accuracy of the results is checked by means of integral relations that hold for steady flows. Author
Distribution Statement:
APPROVED FOR PUBLIC RELEASE