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