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Investigation of Dynamic Flight Maneuvers With an Iced TailplaneA detailed analysis of two of the dynamic maneuvers, the pushover and elevator doublet, from the NASA/FAA Tailplane Icing Program are discussed. For this series of flight tests, artificial ice shapes were attached to the leading edge of the horizontal stabilizer of the NASA Lewis Research Center icing aircraft, a DHC-6 Twin Otter. The purpose of these tests was to learn more about ice-contaminated tailplane stall (ICTS), the known cause of 16 accidents resulting in 139 fatalities. The pushover has been employed by the FAA, JAA and Transport Canada for tailplane icing certification. This research analyzes the pushover and reports on the maneuver performance degradation due to ice shape severity and flap deflection. A repeatability analysis suggests tolerances for meeting the required targets of the maneuver. A second maneuver, the elevator doublet, is also studied.
Document ID
19990018600
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
VanZante, Judith Foss
(DYNACS Engineering Co., Inc. Brook Park, OH United States)
Ratvasky, Thomas P.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1999
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:208849
NASA/TM-1999-208849
E-11470
AIAA Paper 99-0371
Report Number: NAS 1.15:208849
Report Number: NASA/TM-1999-208849
Report Number: E-11470
Report Number: AIAA Paper 99-0371
Meeting Information
Meeting: Aerospace Sciences
Location: Reno, NV
Country: United States
Start Date: January 11, 1999
End Date: January 14, 1999
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS3-9808
PROJECT: RTOP 548-20-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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