Higher-Order Temporal Schemes with Error Controllers for Unsteady Navier-Stokes Equations

Author:

Vatsa Veer1,Carpenter Mark1

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference30 articles.

1. 1Sawada,K.andTakanashi,S. "AnumericalInvestigationofWing/NacelleInterferencesofUSBConfigurations."AIAAPaper87-0455,Jan.1987.

2. 2Yu,N.J.,Chen,H.C.,andSummerfield,D.M. "FlowSimulationsforaComplexAirplaneConfigurationusingEulerEquations."AIAAPaper87-0454, Jan.1987.

3. 3Jameson,A.,Baker,T.J.,andWeatherill,N.P. "CalculationofInviscidFlowOveraCompleteAircraft."AIAAPaper86-0103,Jan.1986.

4. 4Reuther, J., Jameson, A., Martinelli, L, and Saunders, D. "Aerodynamic shape optimization of complex configurations via an adjoint formulation." AIAAPaper96-0091,Jan.1996.

5. 5Buning,P.G.'Obayashi,R.M.,rizk,Y.M.,andSteger,J.L. "NumericalSimulationofIntegratedSpaceShuttleVehicleinAscent."AIAAPaper88-4359 CP,Aug.1988.

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