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Computation of Unsteady Nonlinear Plows in Cascades Using a Harmonic Balance Technique
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Hall, K. C., Thomas, J. P., Clark, W. S., "Computation of Unsteady Nonlinear Plows in Cascades Using a Harmonic Balance Technique", AIAA Journal, Vol. 40, No. 5, 2002, pp. 879-886.
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Hall, K.C.1
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0036531499
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Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter and Limit Cycle Oscillations
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Thomas, J. P., Dowell, E. H., Hall, K. C., "Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter and Limit Cycle Oscillations", AIAA Journal, Vol. 40, No. 4, 2002, pp. 638-646.
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Thomas, J.P.1
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0036079066
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Modeling Viscous Transonic Limit Cycle Oscillation Behavior Using a Harmonic Balance Approach
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Denver, CO, April
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Thomas, J. P., Dowell, E. H., Hall, K. C., "Modeling Viscous Transonic Limit Cycle Oscillation Behavior Using a Harmonic Balance Approach", AIAA Paper 2002-1414, 43th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Denver, CO, April 2002.
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AIAA Paper 2002-1414, 43th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference
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Thomas, J.P.1
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0032269567
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Recipes for Adjoint Code Construction
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Giering, R.1
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Applying TAP to a Navier-Stokes Solver that Simulates an Euler Plow Around an Airfoil
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Currently in Press, Publisher Elsevier, Amsterdam
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Giering, R., Kaminski, T., Slawig, T. ", "Applying TAP to a Navier-Stokes Solver that Simulates an Euler Plow Around an Airfoil", Future Generation Computer Systems, Currently in Press, Publisher Elsevier, Amsterdam, 2002.
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Recent Improvements in Aerodynamic Design Optimization on Unstructured Meshes
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January, Reno, NV
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Xielseti. E. J., Anderson, W. K., "Recent Improvements in Aerodynamic Design Optimization on Unstructured Meshes", AIAA Paper 2001-0596, 39th AIAA Aerospace Sciences Meeting and Exhibit, January, 2001, Reno, NV.
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AIAA Paper 2001-0596, 39th AIAA Aerospace Sciences Meeting and Exhibit
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Xielseti, E.J.1
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Sensitivity Analysis of Unsteady Inviscid Plow Through Turbomachinery Cascades
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Plorea, R., Hall, K. C., "Sensitivity Analysis of Unsteady Inviscid Plow Through Turbomachinery Cascades", AIAA Journal, Vol. 39, No. 6, 2001, pp. 1047-1057.
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Plorea, R.1
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Adjoint Code Developments Using the Exact Discrete Approach
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June, Anaheim, CA
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Giles, M. B., Duta, M. C., Müller, J., D., "Adjoint Code Developments Using the Exact Discrete Approach", AIAA Paper 2001-0596, 15th Computational Fluid Dynamics Conference, June, 2001, Anaheim, CA.
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AIAA Paper 2001-0596, 15th Computational Fluid Dynamics Conference
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Giles, M.B.1
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Acceleration of Convergence to Period Steady State in Turbomachinery Plows
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January, Reno, NV
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McMullen, M., Jameson, A., Alonso, J. J., "Acceleration of Convergence to Period Steady State in Turbomachinery Plows", AIAA Paper 2001-0152, 39th AIAA Aerospace Sciences Meeting and Exhibit, January, 2001, Reno, NV.
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McMullen, M.1
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Application of a Non-Linear Frequency Domain Solver to the Euler and Navier-Stokes Equations
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January, Reno, NV
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McMullen, M., Jameson, A., Alonso, J. J., "Application of a Non-Linear Frequency Domain Solver to the Euler and Navier-Stokes Equations", AIAA Paper 20020120, 40th AIAA Aerospace Sciences Meeting and Exhibit, January, 2002, Reno, NV.
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AIAA Paper 20020120, 40th AIAA Aerospace Sciences Meeting and Exhibit
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McMullen, M.1
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13
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A Multiple Grid Scheme for Solving the Euler Equations
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Spalart, P. R., and Allmaras, S. R., "A One Equation Turbulence Model for Aerodynamic Plows", AIAA Paper 92-0439, January, 1992.
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A One Equation Turbulence Model for Aerodynamic Plows
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Spalart, P.R.1
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Experiments on Transonic Flutter of a Two-Dimensional Supercritical Wing with Emphasis on Non-Linear Effects
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London, UK, July 17-18
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Schewe, G., Deyhle, H., "Experiments on Transonic Flutter of a Two-Dimensional Supercritical Wing with Emphasis on Non-Linear Effects", Proceeding of the Royal Aeronautical Society Conference on Unsteady Aerodynamics, London, UK, July 17-18, 1996.
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English Version (Translated by Dr. W. F. King III), German Aerospace Center DLR Pinal Report Number DLR IB 232-2002 J 01, Corresponds to Pinal Report for BMBP: Nichtlineare Effekte beim transsonischen Flattern (PKZ 13 N 7172), and Internal Report DLR IB 2001 J03, January 25
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Schewe, G., Knipfer, A., Mai, H., Dietz, G., "Experimental and Numerical Investigation of Nonlinear Effects in Transonic Flutter", English Version (Translated by Dr. W. F. King III), German Aerospace Center DLR Pinal Report Number DLR IB 232-2002 J 01, Corresponds to Pinal Report for BMBP: Nichtlineare Effekte beim transsonischen Flattern (PKZ 13 N 7172), and Internal Report DLR IB 2001 J03, January 25, 2002.
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Experimental and Numerical Investigation of Nonlinear Effects in Transonic Flutter
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Schewe, G.1
Knipfer, A.2
Mai, H.3
Dietz, G.4
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84982317999
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Investigations of an Oscillating Supercritical 2D Wing Section in Transonic Flow
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Reno, NV, January
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Knipfer, A., Schewe, G., "Investigations of an Oscillating Supercritical 2D Wing Section in Transonic Flow", AIAA Paper 98-0653, 36th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1998.
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Knipfer, A.1
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