بررسی تحلیلی جذب انرژی ورق‌های ساندویچی با هسته لانه زنبوری

[1] Hoo Fatt, M.S.; K.S. Park, 2000. “Perforation of honeycomb sandwich plates by projectiles”,

Composites Part A: Applied Science and Manufacturing, 31, No. 8, pp. 889-899.

[2] Backman, M.E.; W. Goldsmith, 1978 . “The mechanics of penetration of projectiles into targets”,International Journal of Engineering Science, 16,No. 1, pp. 1-99.

[3] Corbett, G.G.; S.R. ReidW. Johnson, 1996. “Impact loading of plates and shells by free-flying projectiles:

A review”, International Journal of Impact Engineering, 18, No. 2, pp. 141-230.

[4] Forrestal, M.J.; K. OkajimaV.K. Luk, 1988. “Penetration of 6061-T651 aluminum targets with

rigid long rods”, Applied Mechanics, 55, No. pp.755-760.

[5]رادمهر، داود؛ لیاقت، غلامحسین؛ فعلی، سعید؛ ”تحلیلفرایندنفوذمایلپرتابههایتغییرشکلپذیردراهداففلزیچندلایه“، نشریه مواد

پرانرژی، دوره 11 ، شماره 7، صفحات 21 - 31 ، 1390 .

[6] Mc Farland, R.K., 1963. “Hexagonal cell structures under post-buckling axial load”, AIAA Journal, 1,No. 6, pp. 1380-1385.

[7] Wierzbicki, T., 1983. “Crushing analysis of metal honeycombs”, International Journal of Impact Engineering, 1, No. 2, pp. 157-174.

[8]لیاقت، غلامحسین؛ صدیقی، مجتبی؛ داغیانی، حمیدرضا؛ علوی نیا، علی؛ ” خرد شدنسازههایلانهزنبوریفلزتحتبارهایشبهاستاتیکی“،نشریه دانشکده فنی، دوره 37 ، شماره 1، صفحات 145 - 186 ، 1382 .

[9] Goldsmith, W.; D.L. Louie, 1995. “Axial perforation of aluminum honeycombs by projectiles”,International Journal of Solids and Structures, 32,No. 8–9, pp. 1017-1046.

[10] Liaghat, G.H.; A.A. Nia; H.R. DaghyaniM. Sadighi,2010. “Ballistic limit evaluation for impact of

cylindrical projectiles on honeycomb panels”, Thin-Walled Structures, 48, No. 1, pp. 55-61.

[11] Sabouri, H.; G.H. Liaghat, 2010. “Comments on the article: “Ballistic impact of GLARE™ fiber–metal

laminates”, by Michelle S. Hoo Fatt, Chunfu Lin,Duane M. Revilock Jr., Dale A. Hopkins [Composite

Structures 61 (2003) 73–88]”, Composite Structures, 92, No. 2, pp. 600-601.

[12] Hoo Fatt, M.S.; D. Sirivolu, 2010. “A wave propagation model for the high velocity impact response of a composite sandwich panel”,International Journal of Impact Engineering, 37, No.2, pp. 117-130.

[13]ضیاء شمامی، مجتبی؛ خدارحمی، حسین؛ واحدی، خداداد؛ پل، محمدحسین؛” بررسیتجربیوعددینفوذپرتابهصلبسرتختدرسازه

ساندویچیباهستهفومآلومینیوم“، نشریه مهندسی مکانیک مدرس،دوره 13 ، شماره 5، صفحات 1- 13 ، 1392 .

[14] Feli, S.; M.H. Namdari Pour, 2012. “An analytical model for composite sandwich panels with honeycomb core subjected to high-velocity impact”,Composites Part B: Engineering, 43, No. 5, pp. 2439-2447.

[15]فعلی، سعید؛ جعفری، سید سجاد؛ ” بررسیتحلیلیسوراخشدنورقهایساندویچیآلومینیوم-فومتحتاثرضرببالستیک“،نشریه مهندسی مکانیک مدرس ، دوره 13 ، شماره 6، صفحات 52 - 59 ، 1392 .

[16] Hazizan, M.A.; W.J. Cantwell, 2003. “The low velocity impact response of an aluminium honeycomb sandwich structure”, Composites Part B:Engineering, 34, No. 8, pp. 679-687.

[17] Goldsmith, W.; G.-T. Wang; K. LiD. Crane,1997. “Perforation of cellular sandwich plates”,International Journal of Impact Engineering, 19, No.5–6, pp. 361-379.

[18] Lin, C.; M.S.H. Fatt, 2006. “Perforation of composite plates and sandwich panels under quasistatic and projectile loading”, Journal of composite materials, 40, No. 20, pp. 1801-1840.

[19] Wen, H.; T. Reddy; S. ReidP. Soden, 1997.“Indentation, penetration and perforation of composite laminate and sandwich panels under quasi-static and projectile loading”, Key Engineering Materials, 141, No. pp. 501-552.

[20] Wu, Q.G.; H.M. Wen; Y. QinS.H. Xin, 2012.“Perforation of FRP laminates under impact by flatnosed

projectiles”, Composites Part B: Engineering,43, No. 2, pp. 221-227.

[21] Shivakumar, K.N.; W. ElberW. IIIG, 1985.“Prediction of impact force and duration due to low velocity impact on circular composite laminates”,Applicatiom Mechanic, 52, No. 3, pp. 674-680.

[22] Timoshenko, S.; S. Woinowsky-KriegerS.Woinowsky, Theory of plates and shells. 2. 1959:McGraw-hill New York.

[23] Łukasiewicz, S., 1976. “Introduction of concentrated loads in plates and shells”, Progress in Aerospace

Sciences, 17, No. pp. 109-146.

[24] Woodward, R.L.; M. De Morton, 1976. “Penetration of targets by flat-ended projectiles”, International

Journal of Mechanical Sciences, 18, No. 3, pp. 119-127.

[25] Hou, W.; F. Zhu; G. LuD.-N. Fang, 2010. “Ballistic impact experiments of metallic sandwich panels with

aluminium foam core”, International Journal of Impact Engineering, 37, No. 10, pp. 1045-1055.

[26] نامداری پور، محمدهادی؛ ”تحلیلصفحاتساندویچیلانهزنبوری-کامپوزیتتحتبارضربهایعمودی“، کارشناسی ارشد، کرمانشاه، دانشگاه رازی، 1390 .

[27] Forrestal, M.J.; V.K. LukN.S. Brar, 1990.“Perforation of aluminum armor plates with conicalnose

projectiles”, Mechanics of Materials, 10, No.1–2, pp. 97-105.

[28] Forrestal, M.J.; K. OkajimaV.K. Luk, 1988.“Penetration of 6061-T651 Aluminum Targets With Rigid Long Rods”, Journal of applied mechanics, 55,No. 4, pp. 755-760.