MIL-STD-1920A(AV). American military standard, light fixed and rotary-wing aircraft crash resistance [S]. 1988.
[2]
FARLEY G L. Energy absorption of composite material and structures [A]. Proc 43rd American Helicopter Society Annual Forum [C]. St Louis USA:1987. 613-627.
[3]
SIGALAS I, et al. Trigger mechanical in energy-absorbing class cloth/epoxy tubes [J]. Composites Science and Technology,1992, 40:265-287.
[4]
SOTIRIS KELLAS. Design, fabrication and testing of a crushable energy absorber for a passive earth entry vehicle [R].NASA/CR 2002-211425.
[5]
POON C. A review of crashworthiness of composite aircraft structures [R]. Ottawa:National Aeronautical Establishment,Aeronautical Note NAE-AN-63, NRC No. 31276, 1990.2:1-34.
[6]
HULL D. Energy absorbing composite structures [J], Sci & Techn Rev, University of Wales, 1988, 3:23-30.