Engine Debris Fuselage Penetration Testing Phase II

Details

• Creators:
  Lundin, Steven J
• Corporate Creators:
  Commander Naval Air Warfare Center (CA)
• Corporate Contributors:
  United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research
• Subject/TRT Terms:
  • Turbine engines
  • Fuselages
  • Foreign object debris
  • Hazard mitigation
• Publication/ Report Number:
  DOT/FAA/AR-01/27, II
• Resource Type:
  Tech Report
• Geographical Coverage:
  United States
• Edition:
  Final Report
• Contracting Officer:
  Emmerling, William; Altobelli, Donald
• Corporate Publisher:
  United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
• Description:
  During October and November 2000 the Naval Air Warfare Center, China Lake conducted a series of simulated uncontained engine failure structural impact tests. A large 12-inch gas gun was used to launch turbojet engine fan blade segments into a narrow-body commercial aircraft fuselage. The impacts were documented and analyzed with high-speed photography. Impact velocities, presented areas, and residual velocities were calculated. These data were then compared to analytic results predicted by the Joint Technical Coordinating Group for Munitions Effectiveness (JTCG/ME) penetration equations. The results are presented in this report.
• Format:
  PDF
• Download URL:
  https://rosap.ntl.bts.gov/view/dot/94015/dot_94015_DS1.pdf
• File Type:
  [PDF - 2.95 MB]
• Collection(s):
  FAA William J. Hughes Technical Center for Advanced Aerospace
• Main Document Checksum:
  urn:sha-512:ed4e58aa83a08905311bd7a57c71e077c7ce0e00157ecdcea619921a2c9cb8edac47b6d87055c590e292b90c8b9ccc985e5d83b44d4216e3bcd24fad8bbf25f5