PAB3D simulations for the CAWAPI F- 16XL

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 9, Issue , 2007, Pages 5913-5937

  Elmiligui, Alaa ^a,d   Abdol Hamid, K S ^b,e   Massey, Steven J ^c,d  

^a ANALYTICAL SERVICES AND MATERIALS INC   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Eagle Aeronautics Inc   (United States)

^d AIAA   (United States)

^e Building 45   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGEBRAIC STRESS MODEL; FLIGHT CONDITIONS; FLIGHT DATA; GRID RESOLUTION;

ANGLE MEASUREMENT; BOUNDARY LAYER FLOW; COMPUTATIONAL FLUID DYNAMICS; MACH NUMBER; SKIN FRICTION; TURBULENCE MODELS;

WINGS;

EID: 34250853516     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (21)

1. Lamar, John E., Obara, Clifford J.; "Review of Cranked-Arrow Wing Aerodynamics Project: Its International Aeronautical Community Role. AIAA Paper 2007-0487, Presented at 45th AIAA Aerospace Presented at 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
2. Lamar, John E., Obara, Clifford J.; Fisher, Bruce D.; and Fisher, David F.: Flight, Wind-Tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds. NASA/TP-2001-210629, February 2001.
3. Wendy B. Lessard: "Subsonic Analysis of 0.04-Scale F-16XL Models Using an Unstructured Euler Code," NASA TP 3597, October 1996
4. Lamar, John E.; Conin, Catherine K.; and Scott, Laura E.: A Review of Steps Taken to Create an International Virtual Laboratory at NASA Langley for Aerodynamic Prediction and Comparison. Prog Aerospace ci, Vol. 40, p. 163-172, 2004.
5. Lamar, John E.; Cronin, Catherine K.; and Scott, Laura E.: Virtual Laboratory Enabling Collaborative Research in Applied Vehicle Technologies. In AVT-123 Symposium on "Flow Induced Unsteady Loads and the Impact on Military Applications", Keynote 2, Budapest, Hungary, April 25-29, 2005.
6. Boelens, O.J.; Goertz, S.; Morton, S.A.; Fritz, W.; and Lamar, J.E.: Description of the F-16XL Geometry and Computational Grids Used in CAW API. AIAA Paper 2007-0488, 45th AIAA Aerospace Presented at 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
7. Boelens, O.J.; Spekreijse, S.P.; Sytsma, H.A.; and de Cock, K.M.J.: Comparison of measured and simulated flow features for the full-scale F-16XL aircraft. AIAA Paper 2007-0489, 45th AIAA Aerospace Presented at 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
8. Badcock, K.J.: Evaluation of Results from a Reynolds Averaged Multiblock Code Against F-16XL Flight Data. AIAA Paper 2007-0490, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
9. Fritz, W.: Hybrid Grid RANS Solutions for the CAW API F-16XL. AIAA Paper 2007-0492, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
10. Morton. S.A.; McDaniels, D.R.; and Cummings, R.M.: F-16XL Unsteady Simulations for the CAWAPI Facet of RTO Task Group AVT-113. AIAA Paper 2007-0493, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
11. Goertz, S. and Jirasek, A.: Unstructured Steady/Unsteady Solutions with Edge for CAWAPI F-16XL at KTH/FOI. AIAA Paper 2007-0678, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
12. Michal, T.; Oser, M.; Mani, M.; and Ross, F.: BCFD Unstructured-Grid Predictions on the F-16XL (CAWAPI) Aircraft. AIAA Paper 2007-0679, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
13. Michal, T.; Oser, M.; Mani, M.; and Ross, F.: BCFD Unstructured-Grid Predictions on the F-16XL (CAWAPI) Aircraft. AIAA Paper 2007-0679, Presented at 45th AIAA Aerospace Presented at 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
14. Davis, M.B.; Reed, C.; and Yagle, P.: Hybrid Grid Solutions on the (CAWAPI) F-16XL Using Falcon v4. AIAA Paper 2007-0680, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
15. Karman, S.; Mitchell, B.; and Sawyer, S.: Unstructured Grid Solutions of CAW API F-16XL by UT SimCenter. AIAA Paper 2007-0681, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
16. Lamar, J.E. and Abdol-Hamid, K.S.: USM3D Unstructured Grid Solutions for CAW API at NASA LaRC. AIAA Paper 2007-0682, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 8-11, 2007.
17. PAB3D Code Manual Originally developed by the Propulsion Aerodynamics Branch, now under cooperative program between the Configuration Aerodynamics Branch, NASA Langley Research Center and Analytical Services & Materials, Inc. Hampton, VA. See http://www.asm-usa.com/software/pab3d.html
18. Abdol-Hamid, K., Pao, S. P., Hunter, C., Deere, K. A., Massey, S. J., and Elmiligui, A. " PAB3D: Its History in the Use of Turbulence Models in the Simulation of Jet and Nozzle Flows", AIAA-2006-489, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006.
19. Massey, S. J., POST Code Manual, See http://www.asm-usa.com/post/
20. Shih, T.H., Zhu, J., and Lumley, J.L. "A New Reynolds Stress Algebraic Equation Model". NASA TM-106644, August 1994.
21. Elmiligui, A., Abdol-Hamid, K., and Hunter, C. "Numerical Investigation Flow in an Over-Expanded Nozzle with Porous Surfaces", AIAA Paper 2005-4159, Tucson, Arizona, 2005