Development of Composite Aerostructure for UAV Application

  • Conference paper
  • First Online:
Advances in Material Science and Engineering

Abstract

Composite material offers excellent high strength-to-weight ratios suitable for UAV structure. This study aims to fabricate and analyse the synthetic fibre structure for the Universiti Tun Hussein Onn Malaysia Cargo Drone (C-Drone) landing gear. The quasi-static compression test was conducted on the S-glass fibre tube and aluminium alloy tube. The tubes with a dimension of 50 mm outer diameter, 3 mm thickness, and 150 mm height were tested on a universal testing machine (UTM). Both materials were compressed up to 30 mm at a 3 mm/min rate following the requirement in ASTM D-3410. The result shows that fibreglass with brittle properties can withstand an amount of load 35% lower and reduced weight up to 10% compared to aluminium alloy. This research proves that composite material such as glass fibre-reinforced plastic (GFRP) can substitute the current material, aluminium alloy 6061-T6, due to its extensive strength-to-weight ratio, low density, and reasonable price in the market.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Subscribe and save

Springer+ Basic
EUR 32.99 /Month
  • Get 10 units per month
  • Download Article/Chapter or Ebook
  • 1 Unit = 1 Article or 1 Chapter
  • Cancel anytime
Subscribe now

Buy Now

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 129.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 169.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free ship** worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Similar content being viewed by others

References

  1. Wade Lanning (2019) What drones are made of? MatMatch. [Online]. Available: https://matmatch.com/blog/what-are-drones-made-of/. Accessed 29 May 2021

  2. Hafizal Hamidon M, Sultan MTH, Hamdan Ariffin A (2019) Investigation of mechanical testing on hybrid composite materials. In: Jawaid M, Thariq M, NBT-FA. in B. Saba Fibre-Reinforced Composites and Hybrid Composites (eds) Woodhead publishing series in composites science and engineering. Woodhead Publishing, pp 133–156

    Google Scholar 

  3. Uzay C, Boztepe MH, Geren N (2016) Impact energy absorption capacity of fiber reinforced polymer matrix (FRP) composites. Conf Int J Arts Sci 09(June):211–220

    Google Scholar 

  4. Kumar IP, Mohite PM, Kamle S (2013) Axial compressive strength testing of single carbon fibres. Arch Mech 65(1):27–43

    Google Scholar 

  5. Babazadeh J, Rahmani K, Hashemi SJ, Sadooghi A (2021) Effect of glass, carbon, and kevlar fibers on mechanical properties for polymeric composite tubes produced by a unidirectional winding method. Mater Res Exp 8(4):045301. https://doi.org/10.1088/2053-1591/abf0ba

    Article  Google Scholar 

  6. Wonderly C, Grenestedt J, Fernlund G, Cěpus E (2005) Comparison of mechanical properties of glass fiber/vinyl ester and carbon fiber/vinyl ester composites. Compos Part B Eng 36(5):417–426. https://doi.org/10.1016/j.compositesb.2005.01.004

    Article  Google Scholar 

  7. Senapati AK, Kumar A, Kumar A (2018) Investigation on mechanical properties of Al-6061 alloy based MMC. IOP Conf Ser Mater Sci Eng 410(1):012016. https://doi.org/10.1088/1757-899X/410/1/012016

    Article  Google Scholar 

  8. Sampath HP, Srinivasa CV, Naik V (2020) Study of quasi-static compression behaviour of hollow tubes made of glass/epoxy composite. IOP Conf Ser Mater Sci Eng 925(1):012045. https://doi.org/10.1088/1757-899X/925/1/012045

    Article  Google Scholar 

  9. Khalid MY, Al Rashid A, Arif ZU, Akram N, Arshad H, Márquez FPG (2021) Characterization of failure strain in fiber reinforced composites: under on-axis and off-axis loading. Crystals 11(2):1–11. https://doi.org/10.3390/cryst11020216

    Article  Google Scholar 

Download references

Acknowledgements

The research was supported by Transdisciplinary Research Grant Scheme Project (TRGS/K136) and Universiti Tun Hussein Onn Malaysia (UTHM) through Geran Kontrak UTHM (Vot H870). The authors would like to thank Ir. Dr. Sallehuddin Shah Bin Ayop and Tc. Afandi Bin Abu Bakar from Jamilus Research Centre (JRC) FKAAB UTHM for allowing the author to use the machine at JRC.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Ahmad Hamdan .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2023 The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.

About this paper

Check for updates. Verify currency and authenticity via CrossMark

Cite this paper

Shahrul Hairi, S.M.F., Saleh, S.J.M.B.M., Hamdan, A., Omar, Z.B. (2023). Development of Composite Aerostructure for UAV Application. In: Emamian, S.S., Awang, M., Razak, J.A., Masset, P.J. (eds) Advances in Material Science and Engineering. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-19-3307-3_34

Download citation

Publish with us

Policies and ethics

Navigation