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1
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20544476549
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Aerodynamic design via control theory
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A. Jameson. Aerodynamic design via control theory. Journal of Scientific Computing, 3:233-260, 1988.
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(1988)
Journal of Scientific Computing
, vol.3
, pp. 233-260
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Jameson, A.1
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2
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0000961379
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Computational aerodynamics for aircraft design
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A. Jameson. Computational aerodynamics for aircraft design. Science, 245:361-371, 1989.
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(1989)
Science
, vol.245
, pp. 361-371
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Jameson, A.1
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4
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0035245857
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A perspective on computational algorithms for aerodynamic analysis and design
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A. Jameson. A perspective on computational algorithms for aerodynamic analysis and design. Progress in Aerospace Sciences, 37:197-243, 2001.
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(2001)
Progress in Aerospace Sciences
, vol.37
, pp. 197-243
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Jameson, A.1
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5
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0347038536
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Aerodynamic shape optimization techniques based on control theory
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CIME (International Mathematical Summer Center), Martina Franca, Italy
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A. Jameson and L. Martinelli. Aerodynamic shape optimization techniques based on control theory. Technical report, CIME (International Mathematical Summer Center), Martina Franca, Italy, 1999.
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(1999)
Technical Report
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Jameson, A.1
Martinelli, L.2
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6
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85085404450
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Computational fluid dynamics for aerodynamic design: Its current and future impact
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AIAA Paper 2001-0538, Reno, NV, January
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J. C. Vassberg and A. Jameson. Computational fluid dynamics for aerodynamic design: Its current and future impact. AIAA paper 2001-0538, AIAA 39th Aerospace Sciences Meeting & Exhibit, Reno, NV, January 2001.
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(2001)
AIAA 39th Aerospace Sciences Meeting & Exhibit
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Vassberg, J.C.1
Jameson, A.2
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8
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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 Paper 2002-0844, Reno, NV, January
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S. Kim, J. J. Alonso, and A. Jameson. 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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(2002)
AIAA 40th Aerospace Sciences Meeting & Exhibit
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Kim, S.1
Alonso, J.J.2
Jameson, A.3
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9
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85086492356
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Aerodynamic shape optimization of wings including planform variables
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AIAA Paper 2002-0210, Reno, Nevada, January
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K. Leoviriyakit and A. Jameson. Aerodynamic shape optimization of wings including planform variables. AIAA paper 2002-0210, 41st Aerospace Sciences Meeting & Exhibit, Reno, Nevada, January 2003.
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(2003)
41st Aerospace Sciences Meeting & Exhibit
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Leoviriyakit, K.1
Jameson, A.2
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10
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2942750760
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Lifting surface design using multidisplinary optimization
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Stanford University Doctoral Dissertation, Stanford, CA
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S. Wakayama. Lifting surface design using multidisplinary optimization. Technical report, Stanford University Doctoral Dissertation, Stanford, CA, 1994.
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(1994)
Technical Report
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Wakayama, S.1
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11
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2942756966
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Design and analysis of optimally-loaded lifting systems
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October
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I. M. Kroo. Design and analysis of optimally-loaded lifting systems. AIAA paper 1984-2507, October 1984.
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(1984)
AIAA Paper
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, Issue.2507
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Kroo, M.1
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12
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85087602839
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An automated method for sensitivity analysis using complex variables
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AIAA Paper 2000-0689, Reno, Nevada, January
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J. R. R. A. Martins, I. M. Kroo, and J. J. Alonso. An automated method for sensitivity analysis using complex variables. AIAA paper 2000-0689, 38th Aerospace Sciences Meeting, Reno, Nevada, January 2000.
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(2000)
38th Aerospace Sciences Meeting
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Martins, J.R.R.A.1
Kroo, I.M.2
Alonso, J.J.3
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13
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2942712384
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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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C. Bischof, A. Carle, G. Corliss, A. Griewank, and P. Hovland. Generating derivative codes from Fortran programs. Internal report MCS-P263-0991, Computer Science Division, Argonne National Laboratory and Center of Research on Parallel Computation, Rice University, 1991.
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Internal Report
, vol.MCS-P263-0991
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Bischof, C.1
Carle, A.2
Corliss, G.3
Griewank, A.4
Hovland, P.5
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14
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84954695021
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Analysis and design of numerical schemes for gas dynamics 1, artificial diffusion, upwind biasing, limiters and their effect on multigrid convergence
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A. Jameson. Analysis and design of numerical schemes for gas dynamics 1, artificial diffusion, upwind biasing, limiters and their effect on multigrid convergence. Int. J. of Comp. Fluid Dyn., 4:171-218, 1995.
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(1995)
Int. J. of Comp. Fluid Dyn.
, vol.4
, pp. 171-218
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Jameson, A.1
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15
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84864361143
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Analysis and design of numerical schemes for gas dynamics 2, artificial diffusion and discrete shock structure
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A. Jameson. Analysis and design of numerical schemes for gas dynamics 2, artificial diffusion and discrete shock structure. Int. J. of Comp. Fluid Dyn., 5:1-38, 1995.
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(1995)
Int. J. of Comp. Fluid Dyn.
, vol.5
, pp. 1-38
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Jameson, A.1
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16
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84982318787
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A gradient accuracy study for the adjoint-based Navier-Stokes design method
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AIAA Paper 1999-0299, Reno, Nevada, January
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S. Kim, J. J. Alonso, and A. Jameson. A gradient accuracy study for the adjoint-based Navier-Stokes design method. AIAA paper 1999-0299, 37th Aerospace Science Meething & Exhibit, Reno, Nevada, January 1999.
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(1999)
37th Aerospace Science Meething & Exhibit
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Kim, S.1
Alonso, J.J.2
Jameson, A.3
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