Numerical analysis of FBG response to blast wave inside shock tube
Author:
Affiliation:
1. Indian Institute of Science
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3062
Reference11 articles.
1. Obed Samuelraj L., Experiments on Varying Intensity Air Blasts in Shock Tubes, (2017), Ph.D. Thesis,Indian Institute of Science.
2. R Sriram, S N Ram, G M Hegde, M M Nayak and G Jagadeesh, `Shock tunnel measurements of surface pressures in shock induced separated flow field using MEMS sensor array', Meas. Sci. Technol. 26, 095301 (2015) doi:10.1088/0957-0233/26/9/095301.
3. Gautam Hegde, Balaji Himakar, Srisha Rao M V, Gopalkrishna Hegde, and S Asokan, `Simultaneous measurement of pressure and temperature in a supersonic ejector using FBG sensors', Meas. Sci. Technol. 33, 125111 (2022) (14pp). doi:10.1088/1361-6501/ac8a0a.
4. [5]Ravid,EShafir,SZilberman,GBerkovic,BGlam,GAppelbaumandAFedotovGefen,`FibreBraggGratingsensorforshock wavediagnostics', JournalofPhysics:ConferenceSeries 500,142029.(2014) doi:10.1088/1742-6596/500/14/142029.
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