Overview of the abrupt wing stall program

Progress in Aerospace Sciences

Volumn 40, Issue 7, 2004, Pages 417-452

  Hall, Robert M ^a   Woodson, Shawn H ^b   Chambers, Joseph R ^c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NAVAL AIR SYSTEMS COMMAND   (United States)

^c BALL AEROSPACE AND TECHNOLOGIES CORP   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIRCRAFT; COMPUTER SIMULATION; DATA REDUCTION; FLIGHT DYNAMICS; PROJECT MANAGEMENT; SIMULATORS; TRANSONIC AERODYNAMICS;

AERODYNAMIC DATA; COMPUTATIONAL STUDIES; FREE-TO-ROLL (FTR); TRANSONIC LATERAL MOTION; WIND-TUNNEL TOOLS;

WINGS;

EID: 13144267786     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.paerosci.2004.10.002     Document Type: Review

References (34)

1. J. Chambers, and R. Hall Historical review of uncommanded lateral-directional motions at transonic conditions AIAA J Aircr 41 3 2004 436 447
2. Mabey D. Unsteady aerodynamics: retrospect and prospect. Aeronaut J R Aeronaut Soc 1999;1-18.
3. Sisk TR. A technique for the assessment of fighter aircraft precision controllability. AIAA Paper 78-1364, 1978.
4. A. Ross Flying aeroplanes in buffet Aeronaut J 81 1977 427 436
5. O'Leary C. Wind-tunnel measurements of lateral aerodynamic derivatives using a new oscillatory rig with results and comparisons for a Gnat aircraft. RAE TR 77159, October 1977.
6. Traven R, Hagan J, Niewoehner R. Solving wingdrop on the F-18E/F Super Hornet, 1998 report to the aerospace profession. Society of Experimental Test Pilots, September 1998. p. 67-84.
7. Fulghum D. Navy narrows F/A-18E/F wing drop options. Aviat Week, 1998;29.
8. Stookesberry D. CFD modeling of the F/A-18E/F abrupt wing stall - a discussion of lessons learned. AIAA-2001-2662, June 2001.
9. Hanley R, Dunaway D, Lawson K. Operational lessons from the F/A-18E/F total flight control integration process. Presented at NATO symposium on active control technology for enhanced performance operational capabilities of military aircraft, land vehicles and sea vehicles, May 8-11, 2000, Braunschweig, Germany.
10. Bauer S, Hernandez G. Reduction of cross-flow shock-induced separation with a porous cavity at supersonic speeds. AIAA 88-2567, June 1988.
11. Wood R, Banks D, Bauer S. Assessment of passive porosity with free and fixed separation on a tangent-Ogive forebody. Presented at the AIAA Atmospheric Flight Mechanics Conference, Hilton Head, South Carolina, August 10-12, 1992. AIAA Paper No. 92-4494.
12. R. Harris March 4 Blue Ribbon Panel II report Inside the Navy 11 10 1998 5 6
13. McMillin S, Hall R, Lamar J. Transonic experimental observations of abrupt wing stall on an F/A-18E model. AIAA-2003-0591, January 2003.
14. D. Schuster, and J. Byrd Transonic unsteady aerodynamics of the F/A-18E under conditions promoting abrupt wing stall AIAA J Aircr 41 3 2004 485 492
15. J. Lamar, R. Hall, F. Capone, and S. McMillin Usefulness of transonic model static data in predicting flight abrupt-wing-stall AIAA J Aircr 41 3 2004 464 473
16. D. Owens, F. Capone, R. Hall, J. Brandon, and J. Chambers Transonic free-to-roll analysis of abrupt wing stall on military aircraft at transonic speeds AIAA J Aircr 41 3 2004 474 484
17. F. Capone, D. Owens, and R. Hall Development of a transonic free-to-roll test capability AIAA J Aircr 41 3 2004 456 463
18. F. Capone, R. Hall, D. Owens, J. Lamar, and S. McMillin Review and recommended experimental procedures for evaluation of abrupt-wing-stall characteristics AIAA J Aircr 41 3 2004 448 455
19. Woodson S, Green B, Chung J, Grove D, Parikh P, Forsythe J. Understanding abrupt wing stall with CFD. AIAA-2003-0592, January 2003.
20. Forsythe J, Woodson S. Unsteady CFD calculations of abrupt wing stall using detached-eddy simulation. AIAA-2003-0594, January 2003.
21. Green B, Ott J. F/A-18C to E wing morphing study for the abrupt wing stall program. AIAA-2003-0925, January 2003.
22. Parikh P, Chung J. A computational study of the abrupt wing stall (AWS) characteristics for various fighter jets: Part I, F/A-18E & F-16C. AIAA-2003-0746, January 2003.
23. Chung J, Parikh P. A computational study of the abrupt wing stall (AWS) characteristics for various fighter jets: Part II, AV-8B and F/A-18C. AIAA-2003-0747, January 2003.
24. Woodson S, Green B, Chung J, Grove D, Parikh P, Forsythe J. Recommendations for CFD procedures for predicting abrupt wing stall. AIAA-2003-0923, January 2003.
25. Kokolios A, Cook S, Niewoehner R. Use of piloted simulation for evaluation of abrupt wing stall characteristics. AIAA-2003-0924, January 2003.
26. Cook S, Chambers J, Kokolios A, Niewoehner R, Owens B, Page A, Roesch M. An integrated approach to assessment of transonic abrupt wing stall for advanced aircraft. AIAA-2003-0926, January 2003.
27. Nguyen L, Yip L, Chambers J. Self-induced wing rock of slender delta wings. AIAA paper AIAA-81-1883, 1981.
28. Hwang C, Pi W. Investigation of steady and fluctuating pressures associated with the transonic buffeting and wing rock of a one-seventh scale model of the F-5A aircraft. NASA Contractor Report 3061, November 1978.
29. Hwang C, Pi W. Some observations on the mechanism of aircraft wing rock. AIAA Paper 78-1456, August 1978.
30. Bore C. Post-stall aerodynamics of the "Harrier" GR1. AGARD-CP-102, Paper 19, Fluid Dynamics of Aircraft Stalling, April 1972.
31. Purser P. Notes on low-lift buffeting and wing dropping at Mach numbers near one. NACA RM L51A30, March 1951.
32. Jones J. Aircraft dynamic response associated with fluctuating flow fields. AGARD Lecture Series No. 74 on Aircraft Stalling and Buffeting, 1975.
33. Shaw D. Pre-stall behavior of combat aircraft. AGARD Lecture Series No. 74 on Aircraft Stalling and Buffeting, 1975.
34. Roesch M, Randall B. Flight test assessment of lateral activity. AIAA-2003-0748, January 2003.