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1
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84983097974
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Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation
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AIAA paper 97-0643, Reno, Nevada, January
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W. K. Anderson and V. Venkatakrishnan. Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation. AIAA paper 97-0643, 35th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 1997.
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35th Aerospace Sciences Meeting and Exhibit
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Anderson, W.K.1
Venkatakrishnan, V.2
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6
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85085404059
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Unsteady flow investigationsin an axial turbine using the massively parallel flow solver tflo
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technical report 01-0529, AIAA paper, Reno, NV, Jan
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J.J. Alonso J. Yao, R. Davis and A. Jameson. Unsteady flow investigationsin an axial turbine using the massively parallel flow solver tflo. technical report 01-0529. AIAA paper, 39th. Aerospace Sciences Meething and Exhibit, Reno, NV, Jan 2001.
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39th. Aerospace Sciences Meething and Exhibit
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Alonso, J.J.1
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Optimum aerodynamic design using CFD and control theory
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AIAA paper 95-1729, San Diego, CA, June
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A. Jameson. Optimum aerodynamic design using CFD and control theory. AIAA paper 95-1729, AIAA 12th Computational Fluid Dynamics Conference, San Diego, CA, June 1995.
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Jameson, A.1
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Studies of alternative numerical optimization methods applied to the brachistochrone problem
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A. Jameson and J. C. Vassberg. Studies of alternative numerical optimization methods applied to the brachistochrone problem. OptiCON 99, 1999.
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Computation of unsteady nonlinear flows in cascades using a harmonic balance technique
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Technical report, Lyon, France, September
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J. P. Thomas K. C. Hall and W. S. Clark. Computation of unsteady nonlinear flows in cascades using a harmonic balance technique. Technical report, 9th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, Lyon, France, September 2000.
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Thomas, J.P.1
Hall, K.C.2
Clark, W.S.3
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12
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85086615843
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Acceleration of convergence to a periodic steady state in turbomachinery flows
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AIAA paper 01-0152, Reno, NV, Jan
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A. Jameson M. McMullen and J. Alonso. Acceleration of convergence to a periodic steady state in turbomachinery flows. AIAA paper 01-0152, 39th. Aerospace Sciences Meething and Exhibit, Reno, NV, Jan 2001.
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Jameson, A.1
McMullen, M.2
Alonso, J.3
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13
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84894380533
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Application of a non-linear frequency domain solver to the euler and navierstokes equations
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AIAA paper 02-0120, Reno, NV, Jan
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A. Jameson M. McMullen and J. Alonso. Application of a non-linear frequency domain solver to the euler and navierstokes equations. AIAA paper 02-0120, 40th. Aerospace Sciences Meething and Exhibit, Reno, NV, Jan 2002.
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McMullen, M.2
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Matthew McMullen. The Application of Non-Linear Frequency Domain Methods to the Euler and Navier-Stokes Equations. Ph.d. dissertation, Department of Aeronautics and Astronautics, Stanford University, Stanford, CA, March 2003.
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McMullen, M.1
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16
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85086612989
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Sonic boom reduction using an adjoint method for wing-body configurations in supersonic flow
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AIAA paper 2002-5547, Atlanta, GA, September
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S. Nadarajah, A. Jameson, and J. J. Alonso. Sonic boom reduction using an adjoint method for wing-body configurations in supersonic flow. AIAA paper 2002-5547, 9th. AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization Conference, Atlanta, GA, September 2002.
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9th. AIAA/ISSMO Symposium On Multidisciplinary Analysis and Optimization Conference
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Nadarajah, S.1
Jameson, A.2
Alonso, J.J.3
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17
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Ph.d. dissertation, Department of Aeronautics and Astronautics, Stanford University, Stanford, CA, January
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Siva Nadarajah. The Discrete Adjoint Approach to Aerodynamic Shape Optimization. Ph.d. dissertation, Department of Aeronautics and Astronautics, Stanford University, Stanford, CA, January 2003.
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Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on parallel computers
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AIAA paper 96-4045, Bellevue, WA, September
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J. Reuther, J.J. Alonso, M.J. Rimlinger, and A. Jameson. Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on parallel computers. AIAA paper 96-4045, 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Bellevue, WA, September 1996.
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6th AIAA/NASA/ISSMO Symposium On Multidisciplinary Analysis and Optimization
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Reuther, J.1
Alonso, J.J.2
Rimlinger, M.J.3
Jameson, A.4
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19
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85086054628
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Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation
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AIAA paper 96-0094, Reno, Nevada, January
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J. Reuther, A. Jameson, J. Farmer, L. Martinelli, and D. Saunders. Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation. AIAA paper 96-0094, 34th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 1996.
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34th Aerospace Sciences Meeting and Exhibit
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Reuther, J.1
Jameson, A.2
Farmer, J.3
Martinelli, L.4
Saunders, D.5
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