F/A-18C to e wing morphing study for the abrupt-wing-stall program

Journal of Aircraft

Volumn 42, Issue 3, 2005, Pages 617-626

  Green, Bradford E ^a,c   Ott, James D ^b,d  

^a NAVAL AIR SYSTEMS COMMAND   (United States)

^b Syst Simulation Dvmt Directorate   (United States)

^c Aviation Engineering Directorate   (United States)

^d NONE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; DENSITY (OPTICAL); DRAG; REYNOLDS NUMBER; VISCOSITY;

ABRUPT-STALL PHENOMENON; AIRCRAFT DRAG COEFFICIENT; DYNAMIC PRESSURE; FREESTREAM DENSITY;

PARAMETER ESTIMATION;

EID: 22544461067     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.2895     Document Type: Article

References (7)

1. Hall, R. M., and Woodson, S. H., "Introduction to the Abrupt Wing Stall Program," Journal of Aircraft, Vol. 41, No. 3, 2004, pp. 425-435.
2. Grove, D. V., Laiosa, J. P., Woodson, S. H., and Stookesberry, D. C., "Computational Fluid Dynamics Study of an Abrupt Wing Stall Phenomena on the F/A-18E," AIAA Paper 2002-1025, Jan. 2002.
3. Lamar, J. E., and Hall, R. M., "AWS Figure of Merit (FOM) Developed Parameters from Static Tests," AIAA Paper 2003-0745, Jan. 2003.
4. Stookesberry, D. C., "CFD Modeling of F/A-18E/F Abrupt Wing Stall - A Discussion of Lessons Learned," AIAA Paper 2001-2662, June 2001.
5. Bush, R. H., Tower, G. D., and Towne, C. E., "WIND: The Production Flow Solver of the NPARC Alliance," AIAA Paper 1998-0935, Jan. 1998.
6. Menter, F. R., "Zonal Two Equation k-ω Turbulence Models for Aerodynamic Flows," AIAA Paper 1993-2906, July 1993.
7. Lyerla, G. W., "F/A-18C Flow Visualization Wind Tunnel Test in AEDC 4-Ft Transonic PWT, Test No. TC-1029+," BOEING-STL 99A0026, The Boeing Company, St. Louis, MO, Aug. 1999.