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Free-to-Roll Investigation of the Pre-Production F/A-18E Powered Approach Wing DropA free-to-roll study of the low-speed lateral characteristics of the pre-production F/A-18E was conducted in the NASA Langley 12-Foot Low-Speed Tunnel. In developmental flight tests the F/A-18E unexpectedly experienced uncommanded lateral motions in the power approach configuration. The objective of this study was to determine the feasibility of using the free-to-roll technique for the detection of uncommanded lateral motions for the pre-production F/A-18E in the power approach configuration. The data revealed that this technique in conjunction with static data revealed insight into the cause of the lateral motions. The free-to-roll technique identified uncommanded lateral motions at the same angle-of-attack range as experienced in flight tests. The cause of the uncommanded lateral motions was unsteady asymmetric wing stall. The paper also shows that free-to-roll data or static force and moment data alone are not enough to accurately capture the potential for an aircraft to experience uncommanded lateral motion.
Document ID
20050177128
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Owens, D. Bruce
(NASA Langley Research Center Hampton, VA, United States)
Bryant, Elaine M.
(Department of the Air Force United States)
Barlow, Jewel B.
(Maryland Univ. College Park, MD, United States)
Date Acquired
September 7, 2013
Publication Date
April 11, 2005
Subject Category
Aerodynamics
Report/Patent Number
AFIT-CI04-1033
AD-A432636
Report Number: AFIT-CI04-1033
Report Number: AD-A432636
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VERTICAL TAIL
LEX (LEADING EDGE EXTENSION)
FTR (FREE TO ROLL)
F/A-18E AIRCRAFT
AFI 35-205/AFIT SUP
TEF (TRAILING EDGE FLAP)
HORIZONTAL TAIL
FIGHTER AIRCRAFT
ANGLE OF ATTACK
FLIGHT TESTING
MOMENTS
INFLIGHT
STATIC LOADS
CONFIGURATIONS
STATICS
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