NASA Langley Impact Dynamics Facility

740374

02/01/1974

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
This paper describes the NASA Langley Impact Dynamics Facility that will be used to crash test full-scale light aircraft under the Joint FAA/NASA General Aviation Crashworthiness Program. The aircraft are crashed into the ground as free bodies, using a pendulum swing method to obtain desired flightpath angles and velocities. The aircraft are unrestrained during impact to obtain realistic reactions. Accelerations and strains of the aircraft structure are measured during impact. The crash sequence and structural deformations are obtained by external and internal camera coverage.
Meta TagsDetails
DOI
https://doi.org/10.4271/740374
Pages
8
Citation
Vaughan, V., and Alfaro-Bou, E., "NASA Langley Impact Dynamics Facility," SAE Technical Paper 740374, 1974, https://doi.org/10.4271/740374.
Additional Details
Publisher
Published
Feb 1, 1974
Product Code
740374
Content Type
Technical Paper
Language
English