Investigation on influence of time on tear behaviour of airship envelope
Source abstract
Abstract
An experimental investigation on tearing behaviour of a coated fabric used in aerostat/airship has been undertaken. The tear tests have been conducted on bi-axial set up and pressurised cylinder. Tear propagation was studied by inducing dynamic tear on a bi-axially stressed coated fabric through a falling dagger. The influence of traverse rates, 1–500 mm/min, on tear strength under uniaxial loading was also studied. Thiele’s empirical equation has been found to fit the data of bi-axial tests and cylinder tests. The instantaneous tear on a bi-axially stressed fabric when left under constant stress for some duration lead to failure of fabric at even 15% lesser than critical tear slit length in about 15 min. The tear strength of the coated fabric was found to be less at 1 mm/min traverse rate while remaining nearly constant for higher rates of traverse. The critical tear length not only depends upon inherent tear strength of material, diameter and pressure of envelope but also on the time for which the tear remains under creep.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Aerospace Engineering and Energy Systems · Structural Analysis and Optimization · Textile materials and evaluations
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
DRDO Aerial Delivery Research and Development Establishment, Agra, Uttar Pradesh, India
Department of Textile Technology, Indian Institute of Technology Delhi, New Delhi, Delhi, India
DMSRDE, Kanpur, Uttar Pradesh, India
References (22)
Show source-provided references
1. http://articles.philly.com/2003-05-21/news/25460291_1_crew-blimp-navy-program (2003, accessed 12 September 2015).
2. www.ntsb.gov/aviationquery/brief.aspx?ev_id=20001211X12779-National Transportation Safety Board (accessed 18 August 2017).
3. www.tc.gc.ca/eng/civilaviation/publications/tp7317-2-98-229-5102.htm (accessed 18 August 2017).
4. www.gogoflorist.com/blog/2012/09/thai-army-airship-to-fly-again/ (2012, accessed 18 August 2017).
5. http://vintageairphotos.blogspot.in/2013/08/slates-strange-dirigible.html (2013, accessed 12 August 2017).
6. Durney GP. Concepts for prevention of catastrophic failure in large aerostats. In: AIAA international meeting and technical display on global technology 2000 , Baltimore, MD, 6–8 May 1980.10.2514/6.1980-819 ↗
7. Airship Design Criteria, Report No. FAA-P-8110-2, US Department of Transportation, Airworthiness Requirements for Airships 1995, www.faa.gov/aircraft/air_cert/design_approvals/airships/airships_regs/media/aceAirshipDesignCriteria.pdf (accessed 18 August 2017).
8. Miller T, Mandel M. Airship envelopes: requirements, materials and test methods. In: AIAA 3rd international airship convention and exhibition 2000 , Friedrichshafen, 1–5 July 2000, AIAA Paper 2000-A19.
9. 10.1177/15280837730030020310.1177/152808377300300203 ↗
10. Lagerquist DR, Keen LB. Structural design of a high altitude super pressure powered aerostat. In: AIAA lighter-than-air technology conference , Snowmass, CO, 15–17 July 1975. AIAA Paper 75-933.10.2514/6.1975-933 ↗
11. 10.1177/15280837810110010310.1177/152808378101100103 ↗
12. Happold E · Struct Eng · 1987 · 65 · 15
13. 10.4028/www.scientific.net/AMR.217-218.14710.4028/www.scientific.net/AMR.217-218.147 ↗
14. 10.1016/S1000-9361(11)60014-910.1016/S1000-9361(11)60014-9 ↗
15. 10.1016/S0263-8223(03)00099-010.1016/S0263-8223(03)00099-0 ↗
16. Yixi L · Ind J Fibre Text Res · 2008 · 33 · 146
17. 10.1007/s10443-016-9515-210.1007/s10443-016-9515-2 ↗
18. 10.1088/1757-899X/137/1/01202410.1088/1757-899X/137/1/012024 ↗
19. 10.1061/(ASCE)MT.1943-5533.000153710.1061/(ASCE)MT.1943-5533.0001537 ↗
20. Jianwen C, Wujun C, Han Z, et al. Fracture failure analysis and bias tearing strength criterion for a laminated fabric. J Ind Text . Epub ahead of print 22 February 2017. DOI: 10.1177/1528083717695839.10.1177/1528083717695839 ↗
21. 10.2514/1.3226410.2514/1.32264 ↗
22. Thiele JR. Approximation of envelope critical slit length. In: 11th AIAA lighter-than-air systems technology conference , Clearwater Beach, FL, 15–18 May 1995; AIAA 95-1620.