Hybrid grid solutions on the (CAWAPI) F-16XL using falcon v4

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 12, Issue , 2007, Pages 8303-8323

  Davis, M Bruce ^a,b   Reed, Christopher L ^a,b   Yagle, Patrick J ^a  

^a FRAUNHOFER IWES   (Germany)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT TEST; FLOW PHYSICS; HYBRID GRID SOLUTIONS; TRANSONIC FLIGHT;

AEROSPACE ENGINEERING; COMPUTATIONAL GEOMETRY; COMPUTER SIMULATION; FLIGHT DYNAMICS; SUPERSONIC AIRCRAFT; WINGS;

COMPUTATIONAL FLUID DYNAMICS;

EID: 34250885725     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Lamar, J.E., Obara, C.J., Fisher, B.D., and Fisher, D.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.
2. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 2007.
3. th AIAA Aerospace Sciences Meeting and Exhibit, Reno NV, January 2007.
4. Roe, P. L., "Characteristic-Based Schemes for the Euler Equations," Annual Review of Fluid Mechanics, Vol. 18, 1986, pp. 337-365.
5. Smith, B. R., "The k-kl Turbulence Model and Wall Layer Model for Compressible Flows," AIAA Paper 90-1483, June 1990.
6. Reed, C. L., Karman, S. L., and Anderson, D. A., "Implementation of Low Speed Preconditioning in the Splitflow Code," AIAA Paper 97-1867, June 1997.
7. Karypis, G. and Kumar, V., "A fast and high quality multilevel scheme for partitioning irregular graphs," SIAM Journal on Scientific Computing, Vol. 20, No. 1, pp. 359-392, 1999.
8. Karman, S.L. Jr., "Unstructured Viscous Layer Insertion Using Linear-Elastic Smoothing," AIAA-2006-0531, January 2006.