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Numerical simulation of small perturbation transonic flowsThe results of a systematic study of small perturbation transonic flows are presented. Both the flow over thin airfoils and the flow over wedges were investigated. Various numerical schemes were employed in the study. The prime goal of the research was to determine the efficiency of various numerical procedures by accurately evaluating the wave drag, both by computing the pressure integral around the body and by integrating the momentum loss across the shock. Numerical errors involved in the computations that affect the accuracy of drag evaluations were analyzed. The factors that effect numerical stability and the rate of convergence of the iterative schemes were also systematically studied.
Document ID
19760015402
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Seebass, A. R.
(Cornell Univ. Ithaca, NY, United States)
Yu, N. J.
(Cornell Univ. Ithaca, NY, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-147155
Report Number: NASA-CR-147155
Accession Number
76N22490
Funding Number(s)
CONTRACT_GRANT: NGR-33-010-057
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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