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A difference method for the numerical calculation of discontinuous solutions of hydrodynamic equations
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85086490897
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How many steps are required to solve the euler equations of steady compressible flow: In search of a fast solution algorithm
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Anaheim, California, June 11-14
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Jameson, A. and Caughey, D. A., "How Many Steps are Required to Solve the Euler Equations of Steady Compressible Flow: In Search of a Fast Solution Algorithm," AIAA paper 2001-2673, 15th AIAA Computational Fluid Dynamics Conference, Anaheim, California, June 11-14 2001.
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AIAA Paper 2001-2673, 15th AIAA Computational Fluid Dynamics Conference
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20344375794
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Aedynamics
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Encyclopedia of Computational Mechanics
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5
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0004275915
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Oxford University Press, 1960, Translated by S.K. Mitter
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Thwaites, B., editor, Incompressible Aerodynamic, Oxford University Press, 1960, Translated by S.K. Mitter.
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Incompressible Aerodynamic
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Thwaites, B.1
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6
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84874344696
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Wing design by numerical optimization
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Hicks, R.M.1
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20544476549
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Aerodynamic design via control theory
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Journal of Scientific Computing
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Jameson, A.1
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10
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0000961379
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Computational aerodynamics for aircraft design
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July
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Jameson, A., "Computational Aerodynamics for Aircraft Design," Science, Vol. 245, July 1989, pp. 361-371.
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Science
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Ph.d. dissertation, Department of Aeronautics and Astronautics, Stanford University, Stanford, CA, January
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Nadarajah, S. K., 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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Nadarajah, S.K.1
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Ph. D. Dissertation, University of California, Davis, Davis, CA, June
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Reuther, J., "Aerodynamic Shape Optimization Using Control Theory," Ph. D. Dissertation, University of California, Davis, Davis, CA, June 1996.
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Aerodynamic Shape Optimization Using Control Theory
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Reuther, J.1
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13
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85088199782
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6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Bellevue, WA, September
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Reuther, J., Alonso, J., Rimlinger, M., and Jameson, A., "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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Reuther, J.1
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14
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0001097695
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Numerical solutions of the euler equations by finite volume methods with runge-kutta time stepping schemes
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January
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Jameson, A., Schmidt, W., and Turkel, E., "Numerical Solutions of the Euler Equations by Finite Volume Methods with Runge-Kutta Time Stepping Schemes," AIAA paper 81-1259, January 1981.
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AIAA Paper
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Jameson, A.1
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15
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0007474852
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Improvements to the aircraft euler method
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AIAA 25th Aerospace Sciences Meeting, Reno, Nevada, January
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Jameson, A. and Baker, T., "Improvements to the Aircraft Euler Method," AIAA paper 87-0452, AIAA 25th Aerospace Sciences Meeting, Reno, Nevada, January 1987.
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AIAA Paper
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Jameson, A.1
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16
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2942748740
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Apects of unstructured grids and finite volume solvers for the euler and navier stokes equations
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AIAA Aerospace Sciences Meeting, Reno, NV, January
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Barth, T. J., "Apects of unstructured Grids and Finite Volume Solvers for the Euler and Navier Stokes Equations," AIAA paper 91-0237, AIAA Aerospace Sciences Meeting, Reno, NV, January 1991.
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AIAA Paper
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17
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Aerodynamic shape optimization of wings including planform variations
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st Aerospace Sciences Meeting &: Exhibit, Reno, Nevada, January
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st Aerospace Sciences Meeting &: Exhibit, Reno, Nevada, January 2003.
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AIAA Paper
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18
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A perspective on computational algorithms for aerodynamic analysis and design
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Jameson, A., "A perspective on computational algorithms for aerodynamic analysis and design," Progress in Aerospace Sciences, Vol. 37, 2001, pp. 197-243.
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Progress in Aerospace Sciences
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Jameson, A.1
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19
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85085776119
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Design optimization of high-lift configurations using a viscous continuous adjoint method
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AIAA 40th Aerospace Sciences Meeting & Exhibit, Reno, NV, January
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Kim, S., Alonso, J. J., and Jameson, A., "Design Optimization of High-Lift Configurations Using a Viscous Continuous Adjoint Method," AIAA paper 2002-0844, AIAA 40th Aerospace Sciences Meeting & Exhibit, Reno, NV, January 2002.
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AIAA Paper 2002-0844
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Kim, S.1
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20
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85067321071
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Viscous aerodynamic shape optimization of wings including planform variables
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st Applied Aerodynamics Conference, Orlando, Florida, June 23-26
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st Applied Aerodynamics Conference, Orlando, Florida, June 23-26 2003.
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AIAA Paper 2003-3498
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22
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0017995820
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Wing design by numerical optimization
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23
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Generating derivative codes from Fortran programs
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Computer Science Division, Argonne National Laboratory and Center of Research on Parallel Computation, Rice University
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24
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84998717557
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Sensitivity derivatives for advanced CFD algorithm and viscous modeling parameters via automatic differentiation
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11th AIAA Computational Fluid Dynamics Conference, Orlando, Florida
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Green, L. L., Newman, P. A., and Haigler, K. J., "Sensitivity derivatives for advanced CFD algorithm and viscous modeling parameters via automatic differentiation," AIAA paper 93-3321, 11th AIAA Computational Fluid Dynamics Conference, Orlando, Florida, 1993.
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Green, L.L.1
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25
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0003782492
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Sensitivity analysis for the navier-stokes equations on unstructured meshes using complex variables
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Norfolk, VA, June
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Anderson, W. K., Newman, J. C., Whitfield, D. L., and Nielsen, E. J., "Sensitivity Analysis for the Navier-Stokes Equations on Unstructured Meshes using Complex Variables," AIAA paper 99-3294, Norfolk, VA, June 1999.
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26
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0034431751
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Simulation based aerodynamic design
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Big Sky, MO, March
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Jameson, A., Martinelli, L., Alonso, J. J., Vassberg, J. C., and Reuther, J., "Simulation Based Aerodynamic Design," IEEE Aerospace Conference, Big Sky, MO, March 2000.
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IEEE Aerospace Conference
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27
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Jameson, A., "Optimum Aerodynamic Design using Control Theory," Computational Fluid Dynamics Review, 1995, pp. 495-528.
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Computational Fluid Dynamics Review
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28
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84983103398
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Optimum aerodynamic design using CFD and control theory
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AIAA 12th Computational Fluid Dynamics Conference, San Diego, CA, June
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Jameson, A., "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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AIAA Paper
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29
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Optimum aerodynamic design using the navier-stokes equations
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Jameson, A., Martinelli, L., and Pierce, N. A., "Optimum Aerodynamic Design Using the Navier-Stokes Equations," Theoret. Comput. Fluid Dynamics, Vol. 10, 1998, pp. 213-237.
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Theoret. Comput. Fluid Dynamics
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30
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0012450704
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proceeding of computational mathematics driven by industrial problems, CIME International Mathematical Summer (Center), Martina Franca, Italy, June 21-27
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Jameson, A. and Martinelli, L., "Aerodynamic Shape Optimization Techniques Based on Control Theory," Lecture notes in mathematics #1739, proceeding of computational mathematics driven by industrial problems, CIME (International Mathematical Summer (Center), Martina Franca, Italy, June 21-27 1999.
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Von Karman Institute For Fluid Dynamics, Brussels, Belgium, Febuary 3-7
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Jameson, A., "Aerodynamic Shape Optimization Using the Adjoint Method," 2002-2003 lecture series at the von karman institute, Von Karman Institute For Fluid Dynamics, Brussels, Belgium, Febuary 3-7 2003.
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2002-2003 Lecture Series at the Von Karman Institute
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Jameson, A.1
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32
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2942710340
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Reduction of the adjoint gradient formula in the continuous limit
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st AIAA Aerospace Sciences Meeting, Reno, NV, January
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st AIAA Aerospace Sciences Meeting, Reno, NV, January 2003.
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AIAA Paper
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33
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Validation of a multigrid method for the reynolds averaged equations
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Martinelli, L. and Jameson, A., "Validation of a Multigrid Method for the Reynolds Averaged Equations," AIAA paper 88-0414, 1988.
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AIAA Paper
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Martinelli, L.1
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34
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84963610742
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A new high resolution scheme for compressible viscous flows with shocks
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To Appear, AIAA 33nd Aerospace Sciences Meeting, Reno, Nevada, January
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Tatsumi, S., Martinelli, L., and Jameson, A., "A new High Resolution Scheme for Compressible Viscous Flows with Shocks," AIAA paper To Appear, AIAA 33nd Aerospace Sciences Meeting, Reno, Nevada, January 1995.
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AIAA Paper
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35
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Exploring the limits of shock-free transonic airfoil design
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Stanford University, Stanford, CA, July
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Harbeck, M., "Exploring the Limits of Shock-free Transonic Airfoil Design," Problems in Aeronautics and Astronautics Report, Stanford University, Stanford, CA, July 2004.
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Problems in Aeronautics and Astronautics Report
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