NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
On some numerical schemes for transonic flow problemsNew second-order-accurate finite-difference approximations for a class of nonlinear PDEs of mixed type, which includes the two-dimensional low-frequency transonic small-disturbance equation (TSD) and full-potential equation (FP), are presented. For the TSD equation, the scheme is implemented via a time-splitting algorithm; the inclusion of flux limiters keeps the total variation nonincreasing and eliminates spurious oscillations near shocks. Global-linear-stability, TVD, and entropy-stability results are proved. Numerical results for the flow over a thin airfoil are presented. Current techniques used to solve the TSD equation may easily be extended to second-order accuracy by this method. For the FP equation, the new scheme requires no subsonic/supersonic switching and no numerical flux biasing. Global linear stability for all values of the Mach number is proved.
Document ID
19890052496
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mostrel, Marco Mosche
(Bell Communications Research, Inc., Piscataway, NJ; California, University Los Angeles, United States)
Date Acquired
August 14, 2013
Publication Date
April 1, 1989
Publication Information
Publication: Mathematics of Computation
Volume: 52
ISSN: 0025-5718
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0025-5718
Accession Number
89A39867
Funding Number(s)
CONTRACT_GRANT: NAG2-70
CONTRACT_GRANT: N00014-86-K-0691
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available