Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft. The first test (Test 1) represented a flare-to-stall emergency or hard landing onto a rigid surface. The second test (Test 2) represented a controlled-flight- into-terrain (CFIT) with a nose down pitch attitude of the aircraft, which impacted onto soft soil. The third test (Test 3) also represented a CFIT with a nose up pitch attitude of the aircraft, which resulted in a tail strike condition. Test 3 was also conducted onto soft soil. These crash tests were performed for the purpose of evaluating the performance of Emergency Locator Transmitters and to generate impact test data for model calibration. Finite element models were generated and impact analyses were conducted to simulate the three impact conditions using the commercial nonlinear, transient dynamic finite element code, LS-DYNA®. The objective of this paper is to summarize test-analysis results for the three full-scale crash tests.

Authors

• Jackson, Karen E. NASA Langley Research Center
• Fasanella, Edwin L. National Inst. of Aerospace
• Littell, Justin D. NASA Langley Research Center
• Annett, Martin S. NASA Langley Research Center
• Stimson, Chad M. NASA Langley Research Center