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Numerical simulations using a dynamic solution-adaptive grid algorithm, with applications to unsteady internal flowsAn investigation into the numerical simulation of unsteady flows is undertaken using a two-stage Runge-Kutta scheme coupled with the dynamic solution-adaptive grid algorithm developed by the authors. The inviscid fluxes are described by a modified Advective Upwind Split Method to eliminate the need for artificial dissipation. A well-documented numerical example containing moving discontinuities is presented that demonstrates the ability of the coupled grid/solver scheme to accurately capture unsteady flowfield phenomena. Applications are to a typical inlet diffuser configuration at Mach 3.0 with excessive back pressure inducing inlet unstart.
Document ID
19920062933
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Benson, Rusty A.
(NASA Headquarters Washington, DC United States)
Mcrae, D. S.
(NASA Headquarters Washington, DC United States)
Edwards, Jack R.
(North Carolina State University Raleigh, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 92-2719
Report Number: AIAA PAPER 92-2719
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: Palo Alto, CA
Country: United States
Start Date: June 22, 1992
End Date: June 24, 1992
Accession Number
92A45557
Funding Number(s)
CONTRACT_GRANT: F49620-92-J-0189
CONTRACT_GRANT: NAGW-1072
Distribution Limits
Public
Copyright
Other

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