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Crash Test of Three Cessna 172 Aircraft at NASA Langley Research Center's Landing and Impact Research FacilityDuring the summer of 2015, three Cessna 172 aircraft were crash tested at the Landing and Impact Research Facility (LandIR) at NASA Langley Research Center (LaRC). The three tests simulated three different crash scenarios. The first simulated a flare-to-stall emergency or hard landing onto a rigid surface such as a road or runway, the second simulated a controlled flight into terrain with a nose down pitch on the aircraft, and the third simulated a controlled flight into terrain with an attempt to unsuccessfully recover the aircraft immediately prior to impact, resulting in a tail strike condition. An on-board data acquisition system captured 64 channels of airframe acceleration, along with acceleration and load in two onboard Hybrid II 50th percentile Anthropomorphic Test Devices, representing the pilot and co-pilot. Each test contained different airframe loading conditions and results show large differences in airframe performance. This paper presents test methods used to conduct the crash tests and will summarize the airframe results from the test series.
Document ID
20160001629
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Littell, Justin D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
February 5, 2016
Publication Date
November 1, 2015
Subject Category
Aircraft Design, Testing And Performance
Air Transportation And Safety
Report/Patent Number
L-20622
NF1676L-22910
NASA/TM-2015-218987
Funding Number(s)
WBS: WBS 736466.01.08.07.55.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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