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...

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Bibliographic Details
Main Authors: Soumya Ranjan Nanda, Sumit Agarwal, Vinayak Kulkarni, Niranjan Sahoo
Format: Article
Language:English
Published: Hindawi Limited 2017-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2017/2010476