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Improvements to embedded shock wave calculations for transonic flow-applications to wave drag and pressure rise predictionsThe numerical solution of a single, mixed, nonlinear equation with prescribed boundary data is discussed. A second order numerical procedure for solving the nonlinear equation and a shock fitting scheme was developed to treat the discontinuities that appear in the solution.
Document ID
19740022516
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Seebass, A. R. (Cornell Univ. Ithaca, NY, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1974
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-139487
Report Number: NASA-CR-139487
Accession Number
74N30629
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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