Structural Response of Transport Airplanes in Crash Situations

Details

• Creators:
  Thomson, Robert G. ; Caiafa, Caesar A.
• Corporate Creators:
  NASA Langley Research Center
• Corporate Contributors:
  United States. National Aeronautics and Space Administration
• Subject/TRT Terms:
  • Crash data
  • Survival
  • Injuries
  • Crashworthiness
  • Crash investigation
• Publication/ Report Number:
  NASA Tr~-85654
• Resource Type:
  Tech Report
• Geographical Coverage:
  United States
• Edition:
  Technical Memorandum
• Corporate Publisher:
  United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
• Abstract:
  This report highlights the results of contractual studies of transport accident data undertaken in a joint research program sponsored by the FAA and NASA. From these accident data studies it was concluded that the greatest potential for improved transport crashworthiness is in the reduction of fire real ted fatalities. Accident data pertaining to fuselage integrity. main landing gear collapse. fuel tank rupture, wing breaks, tearing of tank lower surfaces, and engine pod scrubbing are discussed. In those accidents where the energy absorbing protective capability of the fuselage structure is expended and the airplane experiences major structural damage, trauma caused fatalities are also discussed. The dynamic performance of current seat/restraint systems are examined but it is concluded that the accident data does not adequately define the relationship between occupant response and the dynamic interaction with the seat, floor and fuselage structure.
• Format:
  PDF
• Download URL:
  https://rosap.ntl.bts.gov/view/dot/92540/dot_92540_DS1.pdf
• File Type:
  [PDF - 4.69 MB]
• Collection(s):
  FAA William J. Hughes Technical Center for Advanced Aerospace
• Main Document Checksum:
  urn:sha-512:37df403a382170f969c8ea2a81606db69713a32e54d9ad692d4d398d8e03000545dc4b89f6e7e42b79bd83d9e9ca7c91d3953d546ad15d2ff5b492cf8b7237c0