Shock Tube as an Impulsive Application Device
Current investigations solely focus on application of an impulse facility in diverse area of high-speed aerodynamics and structural mechanics. Shock tube, the fundamental impulse facility, is specially designed and calibrated for present objectives. Force measurement experiments are performed on a h...
Main Authors: | Soumya Ranjan Nanda, Sumit Agarwal, Vinayak Kulkarni, Niranjan Sahoo |
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Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2017-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2017/2010476 |
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