《轻质点阵材料力学-6.pdf》由会员分享，可在线阅读，更多相关《轻质点阵材料力学-6.pdf（9页珍藏版）》请在taowenge.com淘文阁网|工程机械CAD图纸|机械工程制图|CAD装配图下载|SolidWorks_CaTia_CAD_UG_PROE_设计图分享下载上搜索。
1、参 考 文 献陈烈民,2005.航天器结构与机构.北京:中国科学技术出版社陈明继,方岱宁。2006,多层吸波材料的传输矩阵法研究,功能材料,37:1056 1058范华林,杨卫.07.轻质高强点阵材料及其力学性能研究进展.力学进展.37:99-112方岱宁,戴政.2008.轻质多功能一体化热防护材料的设计杜善义.朱嘉琦,第卜 五属全国复合材料学术会议论文集.北京:国防业出版社:1173 1178方岱宁,郭海成,h AK,等.04。轻质点阵材料的力学行为分析中国力学学会.首属舍国航空航天领域中的力学问题学术研讨会论文集(下册),北京:22-24刘旭红,黄两成,陈裕泽.等,07。强动载荷下金属材料
2、塑性变形本构模型评述。力学进展,37(3):3 6 1 3 7 4钱炜祺,蔡金狮.00再人航天 机表面热流密度辨识,宇航学报,21:1-6沈观林。1996,复合材料力学。北京:清华大学出版社工斌。2008,轻质点阵结构的多功能优化设计 E博士学位论文.北 京:清华大学王礼立.05.应力波基础。北京:国防I业出版社温熙森。06。光子/声子晶体理论与技术。北京:科学出版社邢丽英。2004,隐身材料。北京:化学工业出版社姚元媛,1999,氧化铝纤维的制造与性能及其在高温炉上的应用.i 业加热,5:42-47甄妮,闰志忠,汪越胜。08,蜂窝材料的弹忤波传播特性.力学学报,(6):769-775周培基,
3、霍普肯斯AK.1985,材料对强冲击载荷的动态响应。北京:科学出版社Ab r a t e S.1998.Im p a c t o n Cm p s i t e St r u c t u r e s.Ne w Yr k:Ca m b r i d g e Un i v e r s i t y Pr e s s丿 e n H()。1969。An a l y s i s a n d De s i g n o f s t r u c t u r a l s a n d w i c h Pa n e l s.Ln d n:Pe r g a m n Pr c s sA n n.1 9 6 5。B u c k
4、 l i n g o f t h i l l w a l l e d c i r c u l a r c i n d e 心。N A S A S p a c e V e h i d e D e s i g n C r i t e h a,NASA SP8o o 7A shby M F,E vans A G,F leck N A,et al。0 o。M etal F oams:A D esign G uide B oston:B utterw o r t h He i n e m a n nBa h e i-El Di n Y A,Dv r a k G J.2o 08。En h a n c e
5、m e n t o f b l a s t r e s i s t a n c e o f s a n d w l c h p h t e s.Co m p o s i t i e s:Pa r t B,39:120-127B 苟an A.1 9 9 5。C onvectin H cat T ransfer。N ew Y()rk:J hn W iley&1 S onsBi a g i R,Ba r t-s n 1i t h H。2o o 7.Im p c r f e c t i n s e n s i t i v i t y o f p y r a n 1i d a l c o r e s a
6、 n d l/x Ji c h s t r u c t u r e s。In t。J。s o h d s St r u c t,44(1415):4690-47o 6Bo r n M,Wo l f E。1959.Pr i n c i p l e s o f()p t i c s:El e c t r o m a g n e t i c h e r y o f Pr o p a g a t i o n,In t e r f e r e n c ea n d Di f f r a c t i o n o f Ii g h t,I。n d o n:Pc r g a m o n Pr e s sBl
7、l d g n 1a n P W.119.1h e Ph y s i c s f Hi g h Pr e s s u r c,In d o n:Ge o r g e Be l l&s n sBu d h n s k y B。1999。()n t h e m i n i r n u m w e i g h t s o f c o m p r e s s i o n s t r u c t u r e s。In t.J.s a l i d s St r u c t.,36:218 轻质 点 阵材料力学与多功能设计3677-3708Chang C CEbcioglu I K.1961.Efiect
8、of cell geometry on the shear modulus and on density ofsandwich panel cores,J.Basic.trng.,83:513 518Chen C-,I-u T J Fleck N A.1999,Effect of imperfections on the yielding of two-dimensionaloams.J.Mech.Phys.Solids.47 12235*2272(lhen(ll-uf JFleck N A.2001.Efect o inclusions and holes on the stiffness
9、and strenqth ofhoneycombs.Int.J.Mech.Sci.,43:487-504Chen M JPei Y M,Fang D N.2009.Computational method or radar absorbing composite latticegrids.Comput.Mater.Sci.,In PressChuang C H,Huang J S.2002.Elastic moduli and plastic collapse strength o hexagonal honey-combs with plateau borders.Int.J.Mech.Sc
10、i.,44:1,BZT-1844Deshpande V S,Fleck N A.2001a.Coilapse of truss core sandwich beams in 3 point bending.Int.J.Solids Struct.,38,6275 6305Deshpande V SAshby M F,Fleck A.2001b.Foam topology bending versus stretching domina-ted architectures.Acta Mater.,49:1035-1040Deshpande V Strleck N A,Ashby M F.2001
11、c.Effective properties of the octet-truss lattice material.J.Mech.Phys.Solids,49:77 47-77 69Dharmasena K P,Wadley H,Xue Z,et al.2OOB.Mechanical response o metallic honeycomb sand,wich panel structures to high-intensity dynamic loading.Int.J.Impact Eng.,35 1063-1074Dittus F W,Boelter L M K.1930.Heat
12、transfer in automobile radiators of the tubular type.Uni-versity of California Publications in Engineering,2t443-46IEvans A G.2001.l-ightweight materials and structures.Mater.Res.Bull.,26J90-797Evans A G,Hutchinson J W,Fleck N A,et al.2001.The topological design of multifunctional cellular metals.Pr
13、og.Mater.Sci.,46:309 327Fan H LFang D N.2009.Enhancement o mechanical properties o hollow strut foams:Analy-sis.Mater.Des.,30:1659-1666Fan H LJin F N,Fang D N.2O0B.Mechanical properties of hierarchical cellular materials:PartI.Analysis.Compos.Sci.Technol.,68:3380-3387Fan H LYang WChao 2M.2007.Microw
14、ave absorbing composite lattice gridsCompos.Sci.Technol.,67 3472-3479Fan H L,Yang W,Wang B,et aI.2006.Design and manuacturing of a composite lattice structurereinforced by continuous carbon fibers,Tsinghua Sci.Technol.,11:515-522Fang D NCui X D,Zhang Y Het al.2OO9.Mechanical properties and design of
15、 lattice compos-ites and structures,/,/Zhao HFleck N A.IUTAM Syrnposium on Mechanical Properties ofCellular Materials.Vol.12.Netherlands:Springer;9 1BFatt M S HPark K S.2000.Perforation of honeycomb sandwich plates by projectiles.Composites:Part A,31:BE9-899Fleck N A,Deshpande V S.2004,The resistanc
16、e o clamped sandwich beams to shock loading.J.参 考文 献 219 Ap p l。Me c h.,71:386一姓 01Fl o s t C,Ro d r l g u e z P,1997.AXAF h y p v e l o c i t y i m p c a c t t e s t r e s u h s Pr o c e e d i n g s o f t h e 2n d Eur p e a n Co n f e r e n c e o n Sp a c e De b r l s,E已、Es CXC,Da n n s t a d t:ESA
17、 s P-393Gi b s o n IJ,As h b y M F,1997。Ce l l u l a r 勘h d s:s t r u c t u r e a n d Pr o p e r t i e s。s e c o n d e d.Ca m b r i d g e:Ca m b r l d g e Un i v e r s i t y Pr e s sGr c n e s t e d t J L。1998,In u e n c e o f w a v y i m p e r f e c t i o n s i n c e l l w a l l s o n e 1a s t i c
18、s t i f f n e s s o f c e 11u l a rs h d s.J。R/Ic c h.Ph y s.o l i d s,46:29-50Gr e n e s t e d t J I2005.On i n t e r a c t l o n s b e t w e e n i m p e r f e c t l o n s i n c e l l u l a r s o l i d s.J。压 a t e r.Sc i,40:5853-5857(;r e n e s t e d t J I,Ta n a k a K。1999。In f l u e n c e o f c e
19、 l l s h a p e v a r i a t i o n s o n e l a s t i c s t i f f n e s s o f c l o s e dc e l l c e l l u l a r s o h d s.s c r.Ma t e r。,40(l):71-77()o 1d s n 1i t h l l T,Sa c k m a n J L。1991.An e x p e r i r n e n t a l s t u d y o f e n e r g y a b s o r p t i o n i n i m p a c t o n s a n d-w k
20、h p h t e s。I,J,Im p a c t En g,12(2):2迮1-262()o l d s m i t h、V,Lo t l l e D.1995.Ax l a l p e r f o r a t i o n o f a l u m i n u m h o n e y c o m b s b y p r o Je c 0l e s.Im.J,s o h d s St r u c t,32:10171046Go l d s n h、V,Wd n g G T,Li K,e t a l。1997。Pe r f o r a t i o n o f c e l l u l a r s
21、a n d w i c h p l a t e s,In t。J,Im p a c tEn g。,19:361-369Gu S,Lu T J,Ev a n s A G.2001,On t h e d e s i g n o t w d i m e n s i o n a l c e l l u l a r m e t a l s f。r c o m b i n e dh e a t d i s s i p a t i o n a n d s t r u c t u r a 11o a d c a p a c i t y,In t。J,He a t 小犭a s s Tr a n s f.,44:
22、2163-2175Gu e s t S D,Hu t c h i n s n J W,2003。()n t b e d e t e l r n i n a c y o f r e p e t i t i v e s t r u c t u r e s.J。Me c h。Ph y s。l i d s,51:383-391H an D Y,T sai S W。0 3。I nterlockedmposite grids design and manufacturing.J。C ompos M at e r,37:287-316Ha r r l n g t o n F。1968,Fi e l d Co
23、 m p u t a t i o n b y Mo m e n t Me t h o d s。Ne w Yo r k:IEEE Pr e s sHo f f m a n n F,Lu TJ,Ho d s o n H P。2003,He t q t t r a n s f e r p e r f o r l n a n c e o f Ka g o m e s t l k l c t u r e s 8t hUK Nc a t l o n a l He a t Tr a n s f e r Co n e r c n c e.Ox f o r d:Pa p e r HX07Hn g i s t、厂
24、,Li n d g r e n M,He l e n i u s R。2002.s o u n d i n s u l a t i o n o f w a l l s a n e x p e r i m e n t a l p a r a m e t r i c s t u d y.c t a Ac u s t,Un i t e d Ac u s t。,88(6):904-923Hu t c h i n s o n J V,Xu e Z,2005。Me t a l s a n d w i c h p l a t e s o p t i m 讫e d f o r p r e s s u r e
25、i m p u l s e s,In t,J.NIe c h。Sc i.,47:545-569H utchinson R G,W icks N,E vans A G,et d。2 0 0 3。K agome plate structures for actuation.ht.J。So h d s St r u c t。,40:69696980Jo n e s N.1971.A t h e o r e t i Ca l s t u d y o f t h e d y n a n 1i c p l a s t i c b e h a v i o r o f b e a m s a n d p l
26、a t e s /i t h f i n i t ed e f 1e c t i o n s。In t.J.s o h d s St r u c t.,7:10071029Ke l s e y S,Ge l l a d y R A,Cl a r k B W。1958。Th e s h e a r l n o d u l u s o f f o h o n e y c o m b c r e s。Ai r c r a f tEn g.,30:294-302K i m T,2 0 0 3.F l u i d o w a n d h e a t t a n s f e r i n a l a t t
27、 i c c f r a m e m a t e 0 a l E P h。D,T h e s i s .C a m b h g e:Ca m b r i d g e Un i v e r s i t y En g i n e e r i n g De p a r t m e n t 220 轻质点阵材料 力学与 多功能设计Kim T.Hodson H P.l,u T J.2001a.Fluid-flow and end wall heat transer characteristics of anultralight latticrframe material.Int.J.Heat Mass
28、Transf.lT,II2g-II4OKim T.Zhao C Y.Hodson H P.et al.20O.lb.C-onvective heat dissipation with lattice-frame mate-rials.Mech.Mater.36,1011-1O2OKnott E F,Shaefer J F.Tuiey M T.1985.Radar Cross Section:lts prediction Measurement andReduction.Dedham MA:Artech House Inc.Kooistra G WDeshpande V S.Wadley H G
29、.2001.Compressive behavior o age hardenable tet-rahedral lattice truss structures made from aluminiurn Acta Mater.52r4229-4237Lee J H.Kim J.2002.Analysis of sound transmission through periodically stifened panels byspace harmonic expansion method.J.Sound Vibr.251(2)r31g-366Lee S E Kang J H.Kim C G.2
30、006.Fabrication and design of multi-layered radar absorbing struc-tures of MWNT-filled glassepoxy piain-weave pos.Struct.,26:397-405Li KGao X l-Subhash G.2005.Effects of cell shape and cell wall thickness variations on theelastic properties of two-dimensional cellular solids.Int.J.Soiids Struc.42,17
31、77-1795Liu TDeng Z C,Lu T 1.2007.Bi-functional optimization of actively cooled,pressurized hollowsandwich cylinders with prismatic cores.J.Mech.Phys.Solids.55,2565-2G02Lu T J Evans A G.2002.Design of a high authority lexural actuator using an electro-strictivepollrner.Sensors and Actuators A.gg:290-
32、296I-u T J.Hutchinson J W.Evans A G.2001.Optimal design of a lexural actuator.J.Mech.Phys.Solids.49:2071-2093Lu T J.Valdevit L.Evans A G.2005.Active cooiing by metallic sandwich structures with period-ic cores.Prog.Mater.Sci.50:789 815Mahfuz H.Thomas T,Rangari V,et al.2006.On the dynamic response of
33、 sandwich compositesand their core materials.Comp.Sci.Tech.66,246r-2472Mathur G P.Tran Bio N,Bolton J S.et al.i992.Sound transmission through stiffened double-panel structures lined with elastic porous materials./Proceedings of the 14th DGLR/AIAAAero-Acoustics Conference.Vol.1.Aachen,l02-105McFarlan
34、d R K.1963.Hexagonal cell structures under post-buckling axial load.AAIA Journal,I:1380-1385McShane G J.Radford D D.Deshpande V S.et al.2006.The response of clamped sandwich plateswith lattice cores subjected to shock loading.Eur.J.Mech.A/Solids.25:2r5 2zgMead D J,Pujara K K.1971.Space-harmonic anal
35、ysis of periodically supported beams,responseto convected random loading.J.Sound Vibr.,14(4),525-541Mohr D 2005.Mechanism based multi-surface plasticity model or ideal truss lattice materials.Int.J.Solids Struct.12:3235-3260Moody L F.1911.Friction facrors for pipe flow.Trans ASME.66:671-681Nia A A.R
36、azavi S B Majzoobi G H.2008.Ballistic limit determination of aluminum honev-combs experimental study.Mat.Sci.Eng.A.lBB:223-280参 考 文 献 221 OhJ HOh K S,Kim C G,et al.2004.Design of radar absorbing structures using glassrepoxycomposite containing carbon black in X band frequency ranges.Composities:Parr
37、 8,35t,19-56Pack D C,Evans W M,James H J.1918.The propagation of shock waves in steel and lead.Proc.Phys.Soc.,60:1Park K Y,i-ee S EKim C G,et aI.2006.Fabrication and electromagnetic characteristics of elec-tromagnetic wave absorbing sandwich structures.Compos.Sci.Technol.,66,576 58.1PenzienJDidrikss
38、on T.1964.Effective shear modulus of honeycomb cellular structure.AIAAJournal,2:531-535Qiu X Deshpande V S,Fleck N A.2003.Finite element analysis of the dynamic response oclamped sandwich beams subject to shock loading.trur.J.Mech.A/Solids,22:801 814Qiu XFleck N A,Deshpande V S.2005.Impulsive loadin
39、g o clamped monolithic and sandwichbeams over a central patch.J.Mech.Phys.Solids,53:1015 1046Radford D D,Deshpande V S,Fleck N A.2005.The use o metal foam projectiles to simulateshock loading on a strucrure.Int.J.Impact Eng.,31(9)t1152-7I71Rathbun H JRadford D D,Xue Z et a1.2006.Performance of metal
40、lic honevcomb core sandwichbeams under shock loading.Int.J.Solids Struct.,43:1716-1763Reddy T Y,Wen H MReid S Ret al.1998.Penetration and perforation of composite sandwichpanels by hemispherical and conical projectiles.J.Press.Vessel Tech.,120,186-191Roach A M,Jones N,Evans K E.1998.The penetration
41、energy o sandwich panel elements undcrstatic and dynamic loading.Part II.Comp.Struct.,42tISS-IS2Ryan SSchaefer F,Desteanis R,et al.2OOB.A ballistic limit equation or hypervelocity impactson composite honeycomb sandwich panel satellite structures.Adv.Space Res.,41,11521166Schaefer F,Schneider E,l-amb
42、ert M.2OO4.Review of ballistic limit equations or CFRP structurewalls of satellites/Proceedings o the 5th International Symposium on Environmental Testing for Space Programmes,ESA-ESTEC.).loordwijk,ESA SP-558Sigalas M M,Economou E N.1992.Elastic and acoustic wave band structure.J.Sound Vibr.,158(2),
43、377-382Silva M J,Hayes W C,Gibson l-J.1995.The effects o non periodic microstructure on the elasticproperties of two-dimensional cellular solids.Int.J.Mech.Sci.,3 7:1 l6 1 II7 7Skvortsov V,Kepler J,Bozhevolnaya E,2003.Energy partition for ballistic penetration of sand-wich panels.I.J.Impact Eng.,28(
44、7)t6g7-716Smith F C.1999.Effective permittivity of dielectric honeycombs.IEE Proceedings-Microwaves,Antennas and Propagation.1,16:55-59S)rnmonds P S.1954.I.arge plastic deformations of beams under blast typeloading/Proceedingsof the Second U.S.National Congress of Applied Mechanics.Michigen,5O5-515S
45、Ymons D D Fleck N A.2008.The imperfection sensitivity of isotropic two-dimensional elastic 222 轻质点 阵材料力学与多功能设计lattices.J.Appl.Mech.,75(5):051011S)rnons D D,Hutchinson R G,Fleck N A.2005a.Actuation of the Kagome doublrlayer grid part1;prediction o performance o the perfect structure.J.Mech.Phys.Solid
46、s53:1855-1874Symons D D,Shieh J,Fleck N A.2005b.Actuation of the Kagome double layer gridpart 2:effectof imperections on the measured and predicted actuation stiffness.J.Mech.Phys.Solids53:1875-1891Sypeck D J Wadley H N G.2OOl.Multifunctional microtruss laminates:textile synthesis andproperties.J.Ma
47、ter.Res.16:890-897Taylor E,Herbert M Vaughan B.et al.1999.Hypervelocity impact on carbon fibre reinorcedplastic/Aluminium honeycomb,comparison with whipple bumper shields.Int.J.ImpactEng.23:883-893Thoma K,Schafer F.Hiermaier S,et al.2004.An approach to achieve progress in spacecratshielding.Adv.Spac
48、e Res.,34:1063-1075ThompsonJ M Tl-ewis G M.1972.On the optimum design of thin-walled compression mcm-bers.J.Mech.Phys.Solids,20:101-109Tian JLu T JHodson H P,et aL.2004a.Thermal hydraulic performance of sandwich structureswith wire mesh cores and embedded heat pipes/13th International Heat Pipe Lion
49、ference.ShanghaiTianJKim T,Lu T J,et al.2004b.The effects of topology upon fluid-ilow and heat-transferwithin cellular copper strucrures.Inr.J.Heat Mass Trans.,47,3I71.3186Tvergaard V.1973.Imperfection-senstivity of a wide integrally stiffened panel under compres-sron.lnl.J.Solrds Slrucr.,9:177-r92V
50、an der Burg M W D,Shulmeister V,Van der Geissen E,et al,1997.On the linear elastic proper-ties of regular and random open-cell foam models.J.Cell.Plastics,33:31-54Vasiliev V V,Razin A F.2006.Anisogrid composite lattice structures or spacecraft and aircratapplications.Clompos.Struct.,76,182-189Vasili