[1] |
GUIDA M, MARULO F, ABRATE S. Advances in crash dynamics for aircraft safety[J]. Progress in Aerospace Sciences, 2018:106-123.
|
[2] |
Boeing Commercial Airplane Company. Statistical summary of commercial jet airplane accidents, Worldwide Operations 1959-2015[R]. Seattle, Washington, D.C.:Aviation Safety Boeing Commercial Airplanes, 2015.
|
[3] |
THOMSON R G, CAIAFA C. Structural response of transport airplanes in crash situations:NASA-TM-85654[R]. Washington,D.C.:NASA, 1983.
|
[4] |
ABRAMOWITZ A, SMITH T G, VU T, et al. Vertical drop test of a narrow-body transport fuselage section with overhead stowage bins:2002-01-2995[R]. Warrendale, PA:SAE, 2002.
|
[5] |
ABRAMOWITZ A, SMITH T G, VU T. Vertical drop test of a narrow-body transport fuselage section with conformable auxiliary fuel tank onboard:DOT/FAA/AR-00/56[R]. Washington, D.C.:FAA, 2000.
|
[6] |
ADAMS A, LANKARANI H M. A modern aerospace modeling approach for evaluation of aircraft fuselage crashworthiness[J]. International Journal of Crashworthiness, 2003, 8(4):401-413.
|
[7] |
PÉREZ GALÁN J L, CLIMENT H, LE PAGE F. Non-linear response of metallic and composite aeronautical fuselage structures under crash loads and comparison with full scale test[R]. Barcelona:Construcciones Aeronáuticas S.A. (CASA) and Centre d'Essais Aeronautique de Toulouse (CEAT), 2000.
|
[8] |
MALHERBE B, LANGRAND B, CHARLES J L, et al. Improvement of crash models of large aeronautical structures[C]//22nd ICAS Congress Harrogate. Bonn:ICAS, 2000.
|
[9] |
HIROKAZU S, HIROMITSU M, KAZUO I, et al. Crashworthiness research on cabin structure at JAXA[C]//5th Triennial International Aircraft Fire and Cabin Safety Research Conference, 2007.
|
[10] |
HIROKAZU S, TAKAHIRA A. Improvements on impact energy absorbing ability of open section short columns:AIAA-2010-2894[R]. Reston, VA:AIAA, 2010.
|
[11] |
HIROKAZU S, MASAKATSU M, TAKAHIRA A. Impact characteristics estimation of channel section short column under axial impact load:AIAA-2007-2023[R]. Reston, VA:AIAA, 2007.
|
[12] |
COLLINS J S, JOHNSON E R. Static and dynamic response of Graphite-Epoxy curved frames[J]. Journal of Composite Materials, 1990, 26(6):792-803.
|
[13] |
PEREZ J, JOHNSON E, BOITNOTT R. Design and test of semicircular composite frames optimized for crashworthiness[C]//AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, & Materials Conference & Exhibit. Reston, VA:AIAA, 2013.
|
[14] |
JONES L, ROBINSON M, FASANELLA E, et al. Experimental and analytical study of the effects of floor location on response of composite fuselage frames:AIAA-1992-2473[R]. Reston, VA:AIAA, 1992.
|
[15] |
KAREN E J, EDWIN L F, SOTIRIS K. Development of a scale model composite fuselage concept for improved crashworthiness[J]. Journal of Aircraft, 2001, 38(1):95-103.
|
[16] |
SOTIRIS K, KAREN E J, LITTELL J D. Full-scale crash test of an MD-500 helicopter with deployable energy absorbers[C]//American Helicopter Society 66th Annual Forum. Alexandria:Vertical Flight Society, 2010.
|
[17] |
MOSTAFA R. Virtual test & simulation[C]//Engineering, Operations & Technology Boeing Research & Technology, 2013.
|
[18] |
HACHENBERG D, LAVINGE V, MAHE M. Crashworthiness of fuselage hybrid structure[C]//Eighth Triennial International Aircraft Fire and Cabin Safety Research Conference (8IARCSFC).Washington, D.C.:FAA, 2016.
|
[19] |
ARNAUDEAU F, MAHE M, DELETOMBE E, et al. Crashworthiness of aircraft composites structures[C]//ASME 2002 International Mechanical Engineering Congress and Exposition. New York:ASME, 2002:31-40.
|
[20] |
DELSART D, PORTEMONT G, WAIMER M. Crash testing of a CFRP commercial aircraft sub-cargo fuselage section[J]. Procedia Structural Integrity, 2016, 2:2198-2205.
|
[21] |
CAPRIO F D, IGNARRA M, MARULO F, et al. De-sign of composite stanchions for the cargo subfloor structure of a civil aircraft[J]. Procedia Engineering, 2016, (167):88-96.
|
[22] |
WIGGENRAAD J F M, SANTORO D, LEPAGE F, et al. Development of a crashworthy composite fuselage concept for a commuter aircraft:NLR-TP-2001-108[R]. Amsterdam:NLR, 2001.
|
[23] |
刘小川, 周苏枫, 马君峰, 等. 民机客舱下部吸能结构分析与试验相关性研究[J]. 航空学报, 2012, 33(12):2202-2210. LIU X C, ZHOU S F, MA J F, et al. Correlation study of crash analysis and test of civil airplane subfloor energy absorption structure[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(12):2202-2210(in Chinese).
|
[24] |
刘小川, 郭军, 孙侠生, 等. 民机机身段和舱内设施坠撞试验及结构适坠性评估[J]. 航空学报, 2013, 34(9):2130-2140. LIU X C, GUO J, SUN X S, et al. Drop test and structure crashworthiness evaluation of civil airplane fuselage section with cabin interiors[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(9):2130-2140(in Chinese).
|
[25] |
LIU X C, GUO J, BAI C, et al. Drop test and crash simulation of a civil airplane fuselage section[J]. Chinese Journal of Aeronautics, 2015, 28(2):447-456.
|
[26] |
任毅如, 向锦武, 罗漳平, 等. 客舱地板斜撑杆对民机典型机身段耐撞性能的影响[J].航空学报, 2010, 31(2):271-276. REN Y R, XIANG J W, LUO Z P, et al. Influence of cabin floor diagonal strut on crashworthiness of typical fuselage section of civil aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(2):271-276(in Chinese).
|
[27] |
REN Y R, XIANG J W. A comparative study of the crashworthiness of civil aircraft with different strut configurations[J]. International Journal of Crashworthiness, 2010, 15(3):321-330.
|
[28] |
郑建强, 向锦武, 罗漳平, 等. 民机机身耐撞性设计的波纹板布局[J]. 航空学报, 2010, 31(7):1396-1402. ZHENG J Q, XIANG J W, LUO Z P, et al. Crashworthiness layout of civi1 aircraft using waved-plate for energy absorption[J]. Acta Aeronautica et Astronautica Sinca, 2010, 31(7):1396-1402(in Chinese).
|
[29] |
ZHENG J Q, XIANG J W, LUO Z P, et al. The crashworthiness design of transport airplane subfloor using foam material[J]. International Journal of Crashworthiness, 2011, 16(4):375-383.
|
[30] |
郑建强, 向锦武, 罗漳平, 等. 民机机身下部结构耐撞性优化设计[J]. 航空学报, 2012, 33(4):640-649. ZHENG J Q,XIANG J W,LUO Z P, et al. Crashworthiness optimization of civil aircraft subfloor structure[J].Acta Aeronautica et Astroautics Sinca,2012, 33(4):640-649(in Chinese).
|
[31] |
MENG F, ZHOU Q, YANG J. Improvement of crashworthiness behavior for simplified structural models of aircraft fuselage[J]. International Journal of Crashworthiness, 2009, 14(1):83-97.
|
[32] |
ZHU X F, FENG Y W, XUE X F, et al. Evaluate the crashworthiness response of an aircraft fuselage section with luggage contained in the cargo hold[J]. International Journal of Crashworthiness, 2017, 22(4):347-364.
|
[33] |
何欢, 陈国平, 张家滨. 带油箱结构的机身框段坠撞仿真分析[J]. 航空学报, 2008, 29(3):627-633. HE H, CHEN G P, ZHANG J B. Crash simulation of fuselage section with fuel tank[J]. Acta Aeronautica et Astroautics Sinca, 2008, 29(3):627-633(in Chinese).
|
[34] |
ZOU T C, MOU H L, FENG Z Y. Research on effects of oblique struts on crashworthiness of composite fuselage sections[J]. Journal of Aircraft, 2012, 49(6):2059-2063.
|
[35] |
MOU H L, ZOU T C, FENG Z Y, et al. Crashworthiness analysis and evaluation of fuselage section with sub-floor composite sinusoidal specimens[J]. Latin American Journal of Solids and Structures, 2016, 13(6):1187-1202.
|
[36] |
MOU H L, XIE J, FENG Z Y, et al. Parametric analysis of composite sinusoidal specimens under quasi-static crushing[J]. The Aeronautical Journal, 2018, 122(1254):1244-1262.
|
[37] |
冯振宇, 解江, 李恒晖, 等. 大飞机货舱地板下部结构有限元建模与适坠性分析[J]. 航空学报, 2019, 40(2):522394. FENG Z Y, XIE J, LI H H, et al. FE modeling and crashworthiness analysis of large aeroplane sub-cargo structure[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(2):522394(in Chinese).
|
[38] |
牟浩蕾, 赵一帆, 刘义, 等. 航空沉头铆钉动态加载试验及失效模式研究[J]. 航空科学技术, 2019, 30(4):69-78. MOU H L, ZHAO Y F, LIU Y, et al. Dynamic loading failure experiment and failure mode analysis of aeronautic countersunk rivets[J]. Aeronautical Science & Technology, 2019, 30(4):69-78(in Chinese).
|
[39] |
Society of Automotive Engineers International. Instrumentation for impact test-Part 1, electronic instrumentation:SAE J211/1[S]. New York:Society of Automotive Engineers International, 2007.
|