Evaluation of results from a reynolds averaged multiblock code against F-16XL flight data

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 9, Issue , 2007, Pages 5896-5912

  Badcock, K J ^a,b  

^a UNIVERSITY OF LIVERPOOL   (United Kingdom)

^b AIAA   (United States)

Author keywords

Block structured; CFD; Vortical flow

Indexed keywords

CODES (STANDARDS); FLIGHT DYNAMICS; REYNOLDS EQUATION; TURBULENCE MODELS; UNSTEADY FLOW; VORTEX FLOW;

FLAPS; FLIGHT MEASUREMENT; TRANSONIC FLIGHT;

WINGS;

EID: 34347211021     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-490     Document Type: Conference Paper

References (16)

1. Illaker, H.J., F-16XL Flight Test Program Overview, AIAA-83-2730, November, 1983.
2. Talty, P.K. and Caughlin, D.J., F-16XL Demonstrates New Capabilities in Flight Test at Edwards Air Force Base, Journal of Aircraft, 25(3), 206-215, 1988.
3. Lamar, J.E., Obara, C.J., Fisher, B.D. and Fisher, D.E., Flight, Wind-tunnel, and Computational Fluid Dynamics Comparison for Cranked Arrow Wing (F-16XL-1) at Subsonic and Transonic Speeds, NASA/TP-2001-210629, 2001.
4. Anders, S.G. and Fischer, M.C., F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment. NASA/TP-1999-209683, 1999.
5. Soemarwoto, B., Boelens, O., Fritz, W., Allan, M., Ceresola, N., and Bueteflsch, K. "Towards the Simulation of Unsteady Maneuvers Dominated by Vortical Flow". AIAA Paper 2003-3528, 2003.
6. Brandsma, F. J., Kok, J. C., Dol, H. S., and Elsenaar, A. "Leading edge vortex flow computations and comparison with DNW-HST wind tunnel data". RTO / AVT Vortex Flow Symposium, Loen, Norway, 2001.
7. Mitchell, A.M., Morton, S.A., Forsythe, J.R. and Cummings, R.M., Analysis of Delta-Wing Vortical Substructures using Detached-Eddy Simulation, AIAA Journal, 44(5), pp 964-972, 2006.
8. 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 Aerospace Sciences Meeting and Exhibit, Reno NV, Jan 8-11, 2007.
9. Osher, S. and Chakravarthy, S. Upwind Schemes and Boundary Conditions with Applications to Euler Equations in General Geometries. Journal of Computational Physics, Vol. 50, pp 447-481, 1983.
10. Van Leer, B. Towards the Ultimate Conservative Conservative Difference Scheme II; Monotonicity and Conservation Combined in a Second Order Scheme. Journal Computational Physics, Vol 14, 361-374, 1974.
11. Jameson, A. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings. AIAA Paper 91-1596, 1991
12. Badcock, K.J., Richards, B.E. and Woodgate, M.A. Elements of Computational Fluid Dynamics on Block Structured Grids using Implicit Solvers. Progress in Aerospace Sciences, vol 36, 2000, pp 351-392.
13. Gordnier, R. E. "Computational study of a turbulent delta-wing flowfleld using two-equation turbulence models". AIAA 96-2076, 1996.
14. Wilcox, D. C. "Turbulence modelling for CFD". DCW Industries, Inc., La Canada, California, 1993.
15. Allan, M. "A CFD Investigation of wind tunnel interference on delta wing aerodynamics". Ph.D. Thesis, University of Glasgow, Glasgow, UK, October 2002.
16. Morton, S.A., McDaniels, D.R. and Cummings, R, F-16XL Unsteady Simulations for the CAWAPI Facet of RTO Task Group AVT-113, AIAA Paper 2007-0493, 45th Aerospace Sciences Meeting and Exhibit, Reno NV, Jan 8-11, 2007.