Processing, Please wait...

  • Home
  • About Us
  • Search:
  • Advanced Search

Growing Science » Engineering Solid Mechanics » Mechanical characterization and static validation of a satellite honeycomb sandwich structure

Journals

  • IJIEC (747)
  • MSL (2643)
  • DSL (668)
  • CCL (508)
  • USCM (1092)
  • ESM (413)
  • AC (562)
  • JPM (271)
  • IJDS (912)
  • JFS (91)
  • HE (32)
  • SCI (26)

ESM Volumes

    • Volume 1 (16)
      • Issue 1 (4)
      • Issue 2 (4)
      • Issue 3 (4)
      • Issue 4 (4)
    • Volume 2 (32)
      • Issue 1 (6)
      • Issue 2 (8)
      • Issue 3 (10)
      • Issue 4 (8)
    • Volume 3 (27)
      • Issue 1 (7)
      • Issue 2 (7)
      • Issue 3 (6)
      • Issue 4 (7)
    • Volume 4 (25)
      • Issue 1 (5)
      • Issue 2 (7)
      • Issue 3 (7)
      • Issue 4 (6)
    • Volume 5 (25)
      • Issue 1 (7)
      • Issue 2 (6)
      • Issue 3 (6)
      • Issue 4 (6)
    • Volume 6 (32)
      • Issue 1 (8)
      • Issue 2 (8)
      • Issue 3 (8)
      • Issue 4 (8)
    • Volume 7 (28)
      • Issue 1 (7)
      • Issue 2 (6)
      • Issue 3 (7)
      • Issue 4 (8)
    • Volume 8 (36)
      • Issue 1 (8)
      • Issue 2 (10)
      • Issue 3 (9)
      • Issue 4 (9)
    • Volume 9 (36)
      • Issue 1 (9)
      • Issue 2 (9)
      • Issue 3 (9)
      • Issue 4 (9)
    • Volume 10 (35)
      • Issue 1 (9)
      • Issue 2 (8)
      • Issue 3 (10)
      • Issue 4 (8)
    • Volume 11 (39)
      • Issue 1 (10)
      • Issue 2 (10)
      • Issue 3 (9)
      • Issue 4 (10)
    • Volume 12 (41)
      • Issue 1 (10)
      • Issue 2 (9)
      • Issue 3 (12)
      • Issue 4 (10)
    • Volume 13 (32)
      • Issue 1 (12)
      • Issue 2 (7)
      • Issue 3 (7)
      • Issue 4 (6)
    • Volume 14 (9)
      • Issue 1 (9)

Keywords

Supply chain management(166)
Jordan(161)
Vietnam(149)
Customer satisfaction(120)
Performance(113)
Supply chain(110)
Service quality(98)
Competitive advantage(95)
Tehran Stock Exchange(94)
SMEs(87)
optimization(86)
Financial performance(83)
Trust(83)
TOPSIS(83)
Sustainability(81)
Job satisfaction(80)
Factor analysis(78)
Social media(78)
Knowledge Management(77)
Artificial intelligence(77)


» Show all keywords

Authors

Naser Azad(82)
Mohammad Reza Iravani(64)
Zeplin Jiwa Husada Tarigan(63)
Endri Endri(45)
Muhammad Alshurideh(42)
Hotlan Siagian(39)
Jumadil Saputra(36)
Dmaithan Almajali(36)
Muhammad Turki Alshurideh(35)
Barween Al Kurdi(32)
Ahmad Makui(32)
Basrowi Basrowi(31)
Hassan Ghodrati(31)
Mohammad Khodaei Valahzaghard(30)
Sautma Ronni Basana(29)
Shankar Chakraborty(29)
Ni Nyoman Kerti Yasa(29)
Sulieman Ibraheem Shelash Al-Hawary(28)
Prasadja Ricardianto(28)
Haitham M. Alzoubi(27)


» Show all authors

Countries

Iran(2183)
Indonesia(1290)
India(787)
Jordan(786)
Vietnam(504)
Saudi Arabia(453)
Malaysia(441)
United Arab Emirates(220)
China(206)
Thailand(153)
United States(111)
Turkey(106)
Ukraine(104)
Egypt(98)
Canada(92)
Peru(88)
Pakistan(85)
United Kingdom(80)
Morocco(79)
Nigeria(78)


» Show all countries

Engineering Solid Mechanics

ISSN 2291-8752 (Online) - ISSN 2291-8744 (Print)
Quarterly Publication
Volume 9 Issue 1 pp. 55-70 , 2021

Mechanical characterization and static validation of a satellite honeycomb sandwich structure Pages 55-70 Right click to download the paper Download PDF

Authors: Ali Aborehab, Mohammed Kassem, Ahmed Farid Nemnem, M. Kamel

DOI: 10.5267/j.esm.2020.5.004

Keywords: Honeycomb sandwich structure, Compressive testing, Flexural testing and static analysis

Abstract: The honeycomb sandwich structures are extensively utilized in the satellite load bearing structure due to their superior mechanical properties. Investigating such structures and establishing their failure map implies the estimation of their equivalent elastic parameters as well as the experimental measurements of their ultimate strengths. Through a comprehensive study, this article discusses thoroughly the mechanical behavior of an aluminum honeycomb structure exposed to flat-wise compressive and flexural testing. Furthermore, an equivalent finite element model, based upon the sandwich theory, is proposed for simulating the elastic behavior of the flexural testing and comparing computational and experimental results. The comparison of results confirms accurately the usage of the sandwich theory and its related shell-volume-shell approach in the efficient modeling of honeycomb sandwich structures. In addition, the aforementioned honeycomb structure is parameterized from the geometry and material perspective. The outcome of such study reveals that the honeycomb core thickness has the greatest influence on the maximum displacement value. In addition, aluminum alloys are optimum choice for facing sheets material of the honeycomb structure.

How to cite this paper
Aborehab, A., Kassem, M., Nemnem, A & Kamel, M. (2021). Mechanical characterization and static validation of a satellite honeycomb sandwich structure.Engineering Solid Mechanics, 9(1), 55-70.

Refrences
Aborehab, A., Kassem, M., Nemnem, A. F., Kamel, M., & Kamel, H. (2020). Configuration design and modeling of an efficient small satellite structure. Engineering Solid Mechanics , 8 (1), 7-20.
Ashab, A., Ruan, D., Lu, G., & Bhuiyan, A. A. (2016). Finite Element Analysis of Aluminum Honeycombs Subjected to Dynamic Indentation and Compression Loads. Materials , 9 (3).
Bianchi, G., Aglietti, G. S., & Richardson, G. (2010). Development of Efficient and Cost-Effective Spacecraft Structures Based on Honeycomb Panel Assemblies. IEEE Aerospace Conference.
Birman, V., & Kardomateas, G. (2018). Review of current trends in research and applications of sandwich structures. Composites Part B , 142, 221-240.
Boudjemai, A., Amri, R., Mankour, A., Salem, H., Bouanane, M., & Boutchicha, D. (2012). Modal analysis and testing of hexagonal honeycomb plates used for satellite structural design. Materials and Design , 35, 266–275.
C365-00. (2000, April). Standard Test Method for Flatwise Compressive Properties of Sandwich Cores. ASTM .
C393-00. (2000). Standard Test Method for Flexural Properties of Sandwich Constructions. ASTM .
Cheng, S., Zhao, B., Xiao, Z., & Xin, Y. (2015). Compression tests on aluminum honeycomband epoxy resin sandwich panels. Emerging Materials Research , 4 (EMR2).
Czechowski, L., Jankowski, J., & Kotełko, M. (2017). Experimental and numerical three-point bending test for sandwich beams. Journal of KONES Powertrain and Transport , 24 (3).
Feraboli, P. (2006). Damage Resistance Characteristics of Thick-Core Honeycomb Composite Panels. 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Newport, Rhode Island.
Fu, J., Luo, H., Wang, W., & Wang, Z. (2017). Dynamic Response Analysis of Solar Array of a Satellite. IEEE 3rd Information Technology and Mechatronics Engineering Conference (ITOEC).
Gibson, L., & Ashby, M. (1997). Cellular Solids : Structure and Properties, 2nd edition. Cambridge: Cambridge University Press.
Grediac, M. (1993). A finite element study of the transverse shear in honeycomb cores. International Journal of Solids and Structures , 30 (13), 1777-1788.
Hao, L., Geng, L., Shangjun, M., & Wenbin, L. (2011). Dynamic Analysis of the Spacecraft Structure on Orbit Made up of Honeycomb Sandwich Plates. IEEE International Conference on Computer Science and Automation Engineering . Shanghai.
HEXCEL-Composites. (1999). HexWeb Honeycomb Attributes and Properties. Hexcel Composites.
Hussain, M., Khan, R., & Abbas, N. (2018). Experimental and computational studies on honeycomb sandwich structures under static and fatigue bending load. Journal of King Saud University–Science .
Jiang, D., Zhang, D., Fei, Q., & Wu, S. (2014). An approach on identification of equivalent properties of honeycomb core using experimental modal data. Finite Elements in Analysis and Design , 90, 84–92.
Kelsey, S., Gellatly, R., & Clark, B. (1958). The shear modulus of foil honeycomb. Aircraft Engineering and Aerospace Technology , 30 (10), 294-302.
Khan, M. K. (2006). Compressive and lamination strength of honeycomb sandwich panels with strain energy calculation from ASTM standards. Journal of aerospace engineering , 220 (5), 375–386.
Kim, B., & Lee, D. L. (2010). Development of a satellite structure with the sandwich T-joint. Composite Structures , 460–468.
Kolopp, A., Rivallant, S., & Bouvet, C. (2013). Experimental study of sandwich structures as armour against medium-velocity impacts. International Journal of Impact Engineering , 61, 24-35.
Li, X., Li, K., Din, Y., Chen, R., & Lu, F. (2016). Inserting Stress Analysis of Combined Hexagonal Aluminum Honeycombs. Shock and Vibration .
Liu, Y., Gao, W., Liu, W., & Hua, Z. (2017). Numerical Analysis and Mechanical Properties of Nomex Honeycomb Core. Proceedings of the ASME 2017 International Mechanical Engineering Congress and Exposition. Tampa, Florida, USA.
Lv, L., Huang, Y., Cui, J., Qian, Y., Ye, F., & Zhao, Y. (2018). Bending properties of three-dimensional honeycomb sandwich structure composites. Textile Research Journal , 88 (17), 2024-2031.
Olsen, T. (2010). Electromechanical Materials Testing Machines. USA.
Rodriguez-Ramirez, J., Castanie, B., & Bouvet, C. (2018). Experimental and numerical analysis of the shear nonlinear behaviour of Nomex honeycomb core. Composite Structures , 193, 121-139.
Roell, Z. ProLine table-top testing machines Z010. Germany.
Sorohan, Ş., Sandua, M., Sandua, A., & Constantinescu, D. M. (2015). Finite element models used to determine the equivalent in-plane properties of honeycombs. DANUBIA ADRIA SYMPOSIUM on Advanced in Experimental Mechanics (DAS 2015). ScienceDirect.
Su, P., Han, B., Zhao, Z., & Zhang, Q. (2018). Three-point bending of honeycomb sandwich beams with facesheet perforations. Acta Mechanica Sinica , 34 (4), 667–675.
Sun, G., Huo, X., Chen, D., & Li, Q. (2017). Experimental and numerical study on honeycomb sandwich panels under bending and in-panel compression. Materials & Design , 133, 154-168.
Sun, W.-Q., & Cheng, W. (2017). Finite element model updating of honeycomb sandwich plates using a response surface model and global optimization technique. Structural and Multidisciplinary Optimization , 121–139.
Vinson, J. R. (2005). Sandwich Structures: Past, Present, and Future. Sandwich Structures 7: Advancing with Sandwich Structures and Materials. Springer, Dordrecht.
Xia, L.-j., Jin, X.-d., & Wang, Y.-b. (2001). The Equivalent Analysis of Honeycomb Sandwich Plates for Satellite Structure. J Shanghai Jiao Tong Univ , 37 (7), 999-1001.
Zhang, T., Yan, Y., Li, J., & Luo, H. (2016). Low-velocity impact of honeycomb sandwich composite plates. Journal of Reinforced Plastics and Composites , 35 (1), 8-32.
  • 0
  • 1
  • 2
  • 3
  • 4
  • 5

Journal: Engineering Solid Mechanics | Year: 2021 | Volume: 9 | Issue: 1 | Views: 1718 | Reviews: 0

Related Articles:
  • Experimental study of the influence of glass microspheres on flexural respo ...
  • Configuration design and modeling of an efficient small satellite structure
  • Edgewise and flatwise compressive behaviour of foam-filled sandwich panels ...
  • Flexural and shear performance of an innovative foam-filled sandwich panel ...
  • Finite element analysis of out-of-plane compressive properties of a honeyco ...

Add Reviews

Name:*
E-Mail:
Review:
Bold Italic Underline Strike | Align left Center Align right | Insert smilies Insert link URLInsert protected URL Select color | Add Hidden Text Insert Quote Convert selected text from selection to Cyrillic (Russian) alphabet Insert spoiler
winkwinkedsmileam
belayfeelfellowlaughing
lollovenorecourse
requestsadtonguewassat
cryingwhatbullyangry
Security Code: *
Include security image CAPCHA.
Refresh Code

® 2010-2026 GrowingScience.Com