Shock Tube as an Impulsive Application Device
Joint Authors
Nanda, Soumya Ranjan
Agarwal, Sumit
Kulkarni, Vinayak
Sahoo, Niranjan
Source
International Journal of Aerospace Engineering
Issue
Vol. 2017, Issue 2017 (31 Dec. 2017), pp.1-12, 12 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2017-04-05
Country of Publication
Egypt
No. of Pages
12
Abstract EN
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 hemispherical test model integrated with the stress wave force balance.
Similar test model is considered for heat transfer measurements using coaxial thermocouple.
Force and heat transfer experiments demonstrated that the strain gauge and thermocouple have lag time of 11.5 and 9 microseconds, respectively.
Response time of these sensors in measuring the peak load is also measured successfully using shock tube facility.
As an outcome, these sensors are found to be suitable for impulse testing.
Lastly, the response of aluminum plates subjected to impulsive loading is analyzed by measuring the in-plane strain produced during deformation.
Thus, possibility of forming tests in shock is also confirmed.
American Psychological Association (APA)
Nanda, Soumya Ranjan& Agarwal, Sumit& Kulkarni, Vinayak& Sahoo, Niranjan. 2017. Shock Tube as an Impulsive Application Device. International Journal of Aerospace Engineering،Vol. 2017, no. 2017, pp.1-12.
https://search.emarefa.net/detail/BIM-1157920
Modern Language Association (MLA)
Nanda, Soumya Ranjan…[et al.]. Shock Tube as an Impulsive Application Device. International Journal of Aerospace Engineering No. 2017 (2017), pp.1-12.
https://search.emarefa.net/detail/BIM-1157920
American Medical Association (AMA)
Nanda, Soumya Ranjan& Agarwal, Sumit& Kulkarni, Vinayak& Sahoo, Niranjan. Shock Tube as an Impulsive Application Device. International Journal of Aerospace Engineering. 2017. Vol. 2017, no. 2017, pp.1-12.
https://search.emarefa.net/detail/BIM-1157920
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1157920