Efficient viscous design of realistic aircraft configurations

29th AIAA Fluid Dynamics Conference

Volumn , Issue , 1998, Pages 1-17

  Campbell, Richard L ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL EFFICIENCY; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL GEOMETRY; FLUID DYNAMICS; GEOMETRY; ITERATIVE METHODS;

AIRCRAFT CONFIGURATIONS; AIRCRAFT DESIGN PROCESS; DESIGN CAPABILITY; GEOMETRY CONSTRAINTS; RELATIVE STRENGTH; SURFACE CURVATURES; UNSTRUCTURED GRID; WEIGHTED AVERAGING;

DESIGN;

EID: 84959358164     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2539     Document Type: Conference Paper

References (31)

1. Jameson, Antony: Re-Engineering the Design Process through Computation. AIAA-97-0641, 1997.
2. Jou, W.H.; Huffman, W.P.; Young, D.P.; Melvin, R.G.; Bieterman, M.B.; Hilmes, C.L.; and Johnson, F.T.: Practical Considerations in Aerodynamic Design Optimization. AIAA-95-1730-CP, 1995.
3. Cao, H.V.; and Blom, G.A.: Navier-Stokes/Genetic Optimization of Multi-Element Airfoils. AIAA-96- 2487,1996.
4. Foster, Norman R; and Dulikravich, George S.: Three-Dimensional Optimization Using Genetic Evolution and Gradient Search Algorithms. AIAA-96-0555, 1996.
5. Ogot, Madara; Aly, Sherif; Pelz, Richard B.; Marconi, Frank; and Siclari, Michael: Stochastic Versus Gradientbased Optimizers for CFD Design. AIAA-96-0332, 1996.
6. Hicks, R.: Wing Design by Numerical Optimization. AIAA-77-1247, 1977.
7. Chang, I-Chung; Torres, Francisco J.; and van Dam, C. P.: Wing Design Code Using Three-Dimensional Euler Equations and Optimization. AIAA-91-3190, 1991.
8. Reuther, J.; Cliff, S.; Hicks, R.; and van Dam, C.P.: Practical design optimization of wing/body configurations using the Euler equations. AIAA-92-2633, 1992.
9. Huffman, W.P.; Melvin, R.G.; Young, D.P.; Johnson, F.T.; Bussoletti, I.E.; Bieterman, M.B.; and Hilmes, Craig L.: Practical Design and Optimization in Computational Fluid Dynamics. AIAA-93-3111, 1993.
10. Burgreen, Greg W.; and Baysal, Oktay: Three- Dimensional Aerodynamic Shape Optimization of Wings Using Sensitivity Analysis. AIAA-94-0094, 1994.
11. Hou, G.J.-W.; Maroju, V.; Taylor, A.C.; Korivi, V.M.; and Newman, P.A.: Transonic Turbulent Airfoil Design Optimization with Automatic Differentiation in Incremental Iterative Forms. AIAA-95-1692, 1995.
12. Reuther, J.; Alonzo, J.J.; Vassberg, J.C.; Jameson, A.; and Martinelli, L.: An Efficient Multiblock Method for Aerodynamic Analysis and Design on Distributed Memory Systems. AIAA-97-1893, 1997.
13. Reuther, J.; Jameson, A.; Alonso, J.J.; Rimlinger, M.J.; and Saunders, D.: Constrained Multipoint Aerodynamic Shape Optimization Using an Adjoint Formulation and Parallel Computers. AIAA-97-0103, 1997.
14. Jameson, A.; Pierce, N.A.; Martinelli, L.: Optimum Aerodynamic Design using the Navier-Stokes Equations. AIAA-97-0101, 1997.
15. Anderson, W. Kyle; and Venkatakrishnan, V.: Aerodynamic Design Optimization on Unstructured Grids with a Continuous Adjoint Formulation. AIAA-97- 0643, 1997.
16. Campbell, Richard L.: An Approach to Constrained Aerodynamic Design With Application to Airfoils. NASA TP 3260, November, 1992.
17. Campbell, Richard L.: Efficient Constrained Design Using Navier-Stokes Codes. AIAA-95-1808, 1995.
18. Naik, D.; Krist, S.; Vatsa, V.; Campbell, R.; Buning, P.; and Gea, L.: Inverse Design of Nacelles Using Multiblock Navier-Stokes Codes. AIAA-95-1820, 1995.
19. Parikh, Paresh: Development of a Modular Aerodynamic Design System based on Unstructured Grids. AIAA-97-0172, 1997.
20. Campbell, Richard L.; and Smith, Leigh A.: A Hybrid Algorithm for Transonic Airfoil and Wing Design. AIAA-87-2552-CP, 1987.
21. Chan, William M.; Rogers, Stuart E.; Nash, Steven M.; and Buning, Pieter G.: Manual for Chimera Grid Tools, Version 0.5. April, 1998. (Available from authors at NASA Ames Research Center, Moffett Field, CA, 94035)
22. Vatsa, V. N.; Sanetrik, M. D.; and Parlette, E. B.: Development of a Flexible and Efficient Multigrid- Based Multiblock Flow Solver. AIAA-93-0677, 1993.
23. Thomas, J.L.; Taylor, S.L.; and Anderson, W.K.: Navier-Stokes Computations of Vortical Flows Over Low Aspect Ratio Wings. AIAA-87-0207, 1987.
24. Abdol-Hamid, K.S.: Application of a Multiblock/ Multizone Code (PAB 3D) for the Three-Dimensional Navier-Stokes Equations. AIAA-91-2155, 1991.
25. Swanson, R.C.; and Turkel, E.: Multistage Schemes With Multigrid for Euler and Navier-Stokes Equations - Components and Analysis. NASA TP 3631, August, 1997.
26. Buning, P. G.; Parks, S. J.; Chan, W. M.; and Renze, K. J.: Application of the Chimera Overlapped Grid Scheme to Simulation of Space Shuttle Ascent Flows. Presented at the 4th International Symposium on Computational Fluid Dynamics, Davis, CA, September 9-12, 1991.
27. Frink, N. T: Assessment of an Unstructured-Grid Method for Predicting 3-D Turbulent Viscous Flows. AIAA-96-0292, 1996.
28. Frink, Neal T; Pirzadeh, Shahyar; and Parikh, Paresh: An Unstructured-Grid Software System for Solving Complex Aerodynamic Problems. NASA CP-3291, May, 1995.
29. Anderson, W.K.; and Bonhaus, D.L.: An Implicit Upwind Algorithm for Computing Turbulent Flows on Unstructured Grids. Computers and Fluids, Vol. 23, No. 1,1994, pp. 1-21.
30. Lovell, D.A.; and Doherty, J.J.: Aerodynamic Design of Aerofoils and Wings Using a Constrained Optimisation Method, ICAS-94-2.1.2,1994.
31. Pirzadeh, S.: Progress Toward a User-Oriented Unstructured Viscous Grid Generator, AIAA-96-0031, 1996.