An edge-based solution-adaptive method applied to the airplane code

34th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1996, Pages

  Biswas, Rupak ^a   Thomas, Scott D ^b   Cliff, Susan E ^a  

^a NASA AMES RESEARCH CENTER   (United States)

^b Sterling Software   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; COST EFFECTIVENESS; FLOW OF FLUIDS; MESH GENERATION;

ADAPTIVE METHODS; AIRCRAFT CONFIGURATIONS; CAPTURE FLOW; COARSENING AND REFINEMENTS; COST EFFECTIVE; DYNAMIC MESH; TETRAHEDRAL MESHES; TRANSONIC WINGS;

SUPERSONIC AIRCRAFT;

EID: 84962173542     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Biswas, R., and Strawn, R. C., "A New Procedure for Dynamic Adaption of Three-Dimensional Unstructured Grids," Applied Numerical Mathematics, Vol. 13, No. 6, 1994, pp. 437-452.
2. Jameson, A., Baker, T. J., and Weatherill, N. P., "Calculation of Inviscid Transonic Flow Over a Complete Aircraft," AIAA Paper 86-0103, AIAA 24th Aerospace Sciences Meeting, Reno, NV, Jan. 1986.
3. Jameson, A., and Baker, T. J., "Improvements to the Aircraft Euler Method," AIAA Paper 87-0452, AIAA 25th Aerospace Sciences Meeting, Reno, NV, Jan. 1987.
4. Barth, T. J., "A 3-D Upwind Euler Solver for Unstructured Meshes," AIAA Paper 91-1548, AIAA 10th Computational Fluid Dynamics Conference, Honolulu, HI, Jun. 1991.
5. Strawn, R. C., Biswas, R., and Garceau, M., "Unstructured Adaptive Mesh Computations of Ro-torcraft High-Speed Impulsive Noise," Journal of Aircraft, Vol. 32, No. 4, 1995, pp. 754-760.
6. Duque, E. P. N., Biswas, R., and Strawn, R. C., "A Solution Adaptive Structured/Unstructured Overset Grid Flow Solver with Applications to Helicopter Rotor Flows," AIAA Paper 95-1766, AIAA 13th Applied Aerodynamics Conference, San Diego, CA, Jun. 1995.
7. Baker, T. J., "Generation of Tetrahedral Meshes Around Complete Aircraft," 2nd International Conference on Numerical Grid Generation in Computational Fluid Dynamics, NASA and Airforce Office of Scientific Research, Dec. 1988.
8. Baker, T. J., "Automatic Mesh Generation for Complex Three-Dimensional Regions Using a Constrained Delaunay Triangulation," Engineering with Computers, Vol. 5, Nos. 3 and 4, 1989, pp. 161-175.
9. Jameson, A., Cliff, S. E., Thomas, S. D., Baker, T. J., and Cheng, W-S., "Supersonic Transport Design on the IBM Parallel System SP2," NASA Computational Aerosciences Workshop, Moffett Field, CA, Mar. 1995.
10. Biswas, R., and Strawn, R. C., "Mesh Quality Control for Multiply-Refined Tetrahedral Grids," Applied Numerical Mathematics, to appear.
11. Thomas, C. L., "Extrapolation of Sonic Boom Pressure Signatures by the Waveform Parameter Method," NASA TN D-6832, Jun. 1972.
12. Cliíf, S. E., and Thomas, S. D., "Euler/Experiment Correlations of Sonic Boom Pressure Signatures," Journal of Aircraft, Vol. 30, No. 5, 1993, pp. 669-675.
13. Schmitt, V., and Charpin, F., "Pressure Distributions on the ONERA-M6-Wing at Transonic Mach Numbers," AGARD Report AR-138, 1979.
14. Melton, J. E, Thomas, S. D., and Cappuccio, G., "Unstructured Euler Flow Solutions using Hexahedral Cell Refinement," AIAA Paper 91-0637, AIAA 29th Aerospace Sciences Meeting, Reno, NV, Jan. 1991.