Supersonic business jet design using a knowledge-based genetic algorithm with an adaptive, unstructured grid methodology

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

  Chung, Hyoung Seog ^a   Choi, Seongim ^a   Alonso, Juan J ^a  

^a STANFORD UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION ALGORITHMS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER AIDED DESIGN; COST BENEFIT ANALYSIS; EMPENNAGES; FIGHTER AIRCRAFT; GENETIC ALGORITHMS; KNOWLEDGE BASED SYSTEMS; SHOCK WAVES; SUPERSONIC AERODYNAMICS;

ACCURATE PERFORMANCE; ADAPTIVE MESHING TECHNIQUES; AERO-DYNAMIC PERFORMANCE; GENETIC ALGORITHM (GAS); GRADIENT INFORMATIONS; KNOWLEDGE-BASED GENETIC ALGORITHMS; OPTIMIZATION ALGORITHMS; SUPERSONIC BUSINESS JETS;

SUPERSONIC AIRCRAFT;

EID: 85067317817     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3791     Document Type: Conference Paper

References (32)

1. National Research Council, High Speed Research Aeronautics and Space Engineering Board Commercial Supersonic Technology: The Way Ahead, National Academy Press, Washington, D.C., 2002.
2. Thomas A. Zang and Lawrence L. Green. "Multidisciplinary Design Optimization Technique: Implications and Opportunities for Fluid Dynamics 30th AIAA Fluid Dynamics Conference, Norfolk, Virginia, AIAA 99-3798, June 1999
3. Jaroslaw Sobieszczanski-Sobieski and Raphael T. Haftka"Multidisciplinary Aerospace Design Optimization: Survey of Recent Developments," 34th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, AIAA 96-0711, January 1996.
4. J. Martin, J. J. Alonso and J. Reuther"High-Fidelity Aero-Structural Design Optimization of a Supersonic Business Jet," 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA 2002-1483, Denver, CO, April 2002.
5. J. Martin and J. J. Alonso"Complete Configuration Aero-Structural Optimization Using a Coupled Sensitivity Analysis Method," 9th AIAA/ISSMO Symposium on Multidisci-plinary Analysis and Optimization, AIAA 2002-5402 Atlanta, GA, September 2002.
6. Resit Unal, Roger A. Lepsch, Jr. and Mark L. McMillin"Response Surface Model Building and Multidisciplinary Optimization Using Overdetermined D-Optimal Designs," 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, AIAA 98-4759, September 1998
7. Anthony A. Giunta and Layne T. Watson "A Comparison of Approximation Modeling Techniques: Polynomial Versus Interpolating Models," 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, St. Louis, Missouri, AIAA 98-4758, September 1998.
8. J. Sacks, W. J. Welch, T. J. Michell, and H. P. Wynn "Design and Analysis of Computer Experiments," Statistical Science Vol 4. No.4, pp. 409-453, 1989
9. Timothy W. Simpson, Timothy M. Mauery, John J. Korte and Farrokh Mistree "Comparison of Response Surface and Kriging Models in the Multidisciplinary Design of an Aerospike Nozzle," 7th AIAA/USAF/NASA/ISSMO Symposium on Mul-tidisciplinary Analysis and Optimization, St. Louis, Missouri, AIAA 98-4755, September 1998
10. D. E. Goldberg Genetic Algorithms for search, optimization, and machine learning, Addison-Wesley, MA, 1989.
11. W. Liu and S. Batill"Gradient-Enhanced Response Surface Approximations Using Kriging Models," 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, AIAA 2002-5456, Atlanta, GA, September 2002.
12. J. R. Koehler and A. B. Owen"Computer Experiments," Handbook of Statistics Vol. 13, pp. 261-308, Elsevier Science, New York, eds. S. Ghosh and C. R. Rao
13. Edward H. Isaaks and R. Mohan Srivastava An Introduction to Applied Geostatistics, Oxford Univ. Press, Oxford, 1989.
14. H. Chung and J. J. Alonso"Using Gradients to Construct Cokriging Approximation Models for High-Dimensional Design Optimization Problems," 40th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2002-0317, Reno, NV, January 2002.
15. H. Chung and J. J. Alonso"Design of a Low-Boom Supersonic Business Jet Using Cokriging Approximation Models," 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, AIAA 2002-5598, Atlanta, GA, September 2002.
16. C. A. Coello Coello and G. T. Pulido "A Micro-Genetic Algorithms for Multiobjective Optimization," Proceedings of the Genetic and Evolutionary Computation Conference(GECCO'2001), 2001.
17. K. Krishnakumar "Micro-genetic algorithms for stationary and non-stationary function optimization," SPIE Proceedings: Intelligent Control and Adaptive Systems, pages 289-296, 1989.
18. D. L. Carroll "Fortran Genetic Algorithm Driver," http://cuaerospace.com/carroll/ga.html, 2001
19. J. J. Alonso, J. R. R. A. Martins, J. J. Reuther, R. Haimes, and C. A. Crawford "High-Fidelity Aero-Structural Design Using a Parametric CAD-Based Model," 16th AIAA Computational Fluid Dynamics Conference, AIAA 2003-3429, Orlando, FL., 2003.
20. J. J. Reuther, J. J. Alonso, J. C. Vassberg, A. Jameson and L. Martinelli. An Efficient Multiblock Method for Aerodynamic Analysis and Design on Distributed Memory Systems. AIAA Paper 97-1893, AIAA Fluid Dynamics Conference. Snowmass, CO. June 1997.
21. James J. Reuther, Antony Jameson, and Juan J. Alonso "Constrained Multipoint Aerodynamic Shape Optimization Using an Adjoint Formulation and Parallel Computers, Parts I and II," Journal of Aircraft Vol 36, No 1, January-February, 1999
22. Kenneth J. Plotkin"PCBoom3 Sonic Boom Prediction Model-Version 1.0e," Wyle Research Report WR 95-22E, October. 1998.
23. Hamies, R. and Follen, G. "Computational Analysis Programming Interface," Proceedings of the 6th International Conference on Numerical Grid Generation in Computational Field Simulations, Greenwich, 1998
24. Gridgen User Manual ver.13, Pointwise, Inc., Bedford, 1998 Centaur System Users' Manual, http://www.centaursoft.com
25. D. J. Mavriplis. Unstructured Mesh Generation and Adap-tivity ICASE 95-26
26. J. Peraire, M. Mahdati, K. Morgan and O. C. Zienkien-wicz Adaptive Remeshing for Compressible Flow Computation Journal of Computational physics, 72:449-466 October, 1987
27. Jameson, T. J. Baker and N. P. Weatherill. Calculation of Inviscid Transonic Flow over a Complete Aircraft. AIAA 10 of 21 Paper 86-0103, 24th Aerosapce Sciences Meeting, January 6-9, 1986, Reno, Nevada
28. T. J. Baker. Mesh Adaptation Strategies for Problems in Fluid Dynamics. Finite Elements in Analysis and Design, Vol. 2 5, 1997, pp. 243-273.
29. M. A. Park. Adjoint-Based, Three-Dimensional Error Prediction and Grid Adaptation. 32nd Fluid Dynamics Conference, June 24-27, 2002, St. Louis, MO
30. R. Lohner. Generation of Unstructured Grids Suitable for RANS Calculations AIAA Paper 99-0662, 1999
31. G. Warren, W. K. Anderson, J. L. Thomas and S. L. Krist Grid Convergence for Adaptive Methods AIAA paper 91-1592, June 1991 Optimization Toolbox For Use with MATLAB, Version 2, The MathWorks, Inc. Mass., July, 2002
32. J. J. Alonso, I. M. Kroo and A. Jameson Proceedings of the DARPA QSP Technical Exchange Meeting 5. December 2001.