Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft

Abstract

The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (ELT) systems. Three Cessna 172 aircraft were acquired to perform crash testing at the NASA Langley Research Center Landing and Impact Research Facility. Full-scale crash tests were conducted in the summer of 2015, and each test article was subjected to severe, but survivable, impact conditions including a flare-to-stall during emergency landing and two controlled-flight-into-terrain scenarios. Finite element analyses were performed to numerically simulate the aircraft response to the crash tests. The first test simulated impacting a concrete surface represented analytically by a rigid plane. Tests 2 and 3 simulated impacting a dirt surface represented analytically by an Eulerian grid of brick elements using a Mohr–Coulomb material model. The objective of this paper is to summarize the test and analysis results for the three full-scale crash tests. Simulation models of the airframe that correlate well with the tests are needed for future studies of alternate ELT mounting configurations.

Authors

• Brian H. Mason Langley Research Center
• Jerry E. Warren Jr. Langley Research Center

Keywords

• Finite Element Analysis
• General Aviation
• Crash Test
• Crash Simulation
• Test and Analysis Correlation
• Aeroplane
• Aerospace Manufacturers
• Aircraft Components and Structure
• Emergency Locator Transmitter
• Controlled Flight into Terrain
• NASA Langley Research Center
• Emergency Landing
• Finite Element Software
• Newtonian Impact Theory