EXPERIMENTAL VERIFICATION OF PROGRAM KRASH -- A MATHEMATICAL MODEL FOR GENERAL AVIATION STRUCTURAL CRASH DYNAMICS
The results of four fully instrumented, full-scale crash tests involving a single-engine, high-wing light airplane are described. The tests were performed under a contract sponsored by the Federal Aviation Administration. The range of impact conditions included initial airplane roll and/or yaw, a nose-down attitude, a flared nose-up attitude and impacts onto a rigid (concrete) and a flexible (soil) surface. Photographs are presented showing the impact conditions, as well as some typical postcrash damage. The crash test models, analyzed using digital computer program KRASH, are described. Typical analysis versus test correlation results as well as a summary correlation for all four crash tests are presented. The application of Program KRASH to assess structural design concepts with regard to crash dynamics characteristics is briefly described.
- For the SAE Meeting April 3-6, 1979.
Warrendale, PA United States 15096
- Whittlin, G
- Ahrens, D J
- BLOEDEL, A W
- Publication Date: 0
- Features: References;
- Pagination: 14 p.
- Society of Automotive Engineers Preprint
- Issue Number: 0
- Publisher: Society of Automotive Engineers (SAE)
- TRT Terms: Air transportation crashes; Aircraft; Applications; Crash phase; Crashes; General aviation; General aviation aircraft; Impact; Impact tests; Mathematical models; Small aircraft; Structural analysis; Testing; Vehicle dynamics
- Old TRIS Terms: Program krash; Structural crash dynamics
- Subject Areas: Aviation; Research; Safety and Human Factors; Vehicles and Equipment;
- Accession Number: 00300337
- Record Type: Publication
- Source Agency: Engineering Index
- Report/Paper Numbers: SAE 790589
- Files: TRIS
- Created Date: Nov 27 1979 12:00AM