The evolution of NPHASE - Euler/Navier-Stokes computations of unsteady two-dimensional cascade flow fields

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American Institute of Aeronautics and Astronautics

Reference40 articles.

1. [I] Huff, Dennis L., Swafford, Timothy W., and Reddy,T.S.R."Euler FlowPredictions for an OscillatingCascadeUsingaHighResolutionWave- Split Scheme,"ASME-91 -198,June 1991.

2. Numerical analysis of flow through oscillating cascade sections

3. [4]Roe, PL. 'Approximate Riemann Solvers, Parameter Vectors,and Difference Schemes,"Journal of Computational Physics, Vol.43, 1981, pp.357- 372. [SIReddy, T.S.R.Bakhle, M.A., Huff, D.L., and Swafford,T.W. "FlutterAnalysis of CascadesUsingaTwoDimensionalEulerSolver,"AIAA-91- 1681, June 1991.

4. [6]Reddy, T.S.R., Bakhle, M.A., Huff, D.L., and Swafford,T.W."Analysis of CascadesUsingaTwo-Dimensional Euler Aeroelastic AIAA-92-2370, April 1992.

5. [7]Reddy, T.S.R., Bakhle, M.A., Huff, D.L., and Swafford,T.W."Flutter AnalysisofSupersonicAxial Flow CascadesUsinga HighResolutionEuler Solver," NASA TechnicalMemorandum 105798,August 1992 [LIMITED DISTRIBUTION UNTIL AU

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