Hypervelocity Impacts on Honeycomb Core Sandwich Panels Filled with Shear Thickening Fluid

被引:34
|
作者
Warren, Justin [1 ]
Cole, Mike [2 ]
Offenberger, Sean [3 ]
Kota, Kalyan Raj [4 ]
Lacy, Thomas E. [4 ]
Toghiani, Hossein [5 ]
Burchell, Mark [2 ]
Kundu, Santanu [5 ]
Pittman, Charles U., Jr. [6 ]
机构
[1] Mississippi State Univ, Dept Aerosp Engn, Ms State, MS 39762 USA
[2] Univ Kent, Ctr Astrophys & Planetary Sci, Canterbury CT2 7NZ, Kent, England
[3] Virginia Polytech Inst & State Univ, Dept Aerosp & Ocean Engn, Blacksburg, VA 24601 USA
[4] Texas A&M Univ, J Mike Walker 66 Dept Mech Engn, College Stn, TX 77843 USA
[5] Mississippi State Univ, Dave C Swaim Sch Chem Engn, Ms State, MS 39762 USA
[6] Mississippi State Univ, Dept Chem, Ms State, MS 39762 USA
关键词
Hypervelocity impacts; Shear-thickening fluids; Sandwich panels;
D O I
10.1016/j.ijimpeng.2020.103803
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The use of honeycomb core sandwich panels filled with a shear thickening fluid (STF) as a component of spacecraft micrometeomid/orbital debris (MMOD) shielding was investigated using hypervelocity impact (HVI) testing. Incorporating a STF into shielding has the potential to reduce damage to the core and the likelihood of back-side facesheet perforation in the event of a HVI. The sandwich panels tested consisted of 1.27 cm thick hexagonal aluminum honeycomb core bonded between 0.064 cm thick aluminum facesheets. The STF displayed a marked rise in viscosity with increasing shear rate above a critical shear rate. It was based on low molecular weight polyethylene glycol (PEG) and hydrophilic fumed silica. Sandwich panel target specimens filled with the STF were subjected to HVIs by 1 mm diameter stainless steel spheres at nominal temperatures of -80 degrees C or 21 degrees C with nominal impact velocities of 4.8 km/s or 6.8 km/s. Additional specimens filled with PEG only were also impacted for comparison. Visual inspections and X-ray computerized tomography were used to assess impact damage. All of the panels experienced perforation of the impacted facesheet, facesheet bulging, localized delamination, and the formation of a cavity in the damaged core. STF-filled panels sustained significantly less damage than PEG-filled panels. None of the STF-filled panels were completely perforated during impact. In contrast, one of the PEG-filled panels impacted at the peak velocity was perforated. The remaining PEG-filled panel sustained substantially more honeycomb core damage and facesheet-core delamination compared to an analogous STF-filled panel. Sandwich panels filled with the STF provide superior HVI mitigation in comparison to panels filled with a Newtonian fluid (i.e., PEG). These experiments show that incorporation of STFs into MMOD shielding components has the potential to dramatically improve the HVI penetration resistance over a broad range of impact velocities and temperatures.
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页数:7
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