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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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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Wiley
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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| _version_ | 1832567703599054848 |
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| author | Soumya Ranjan Nanda Sumit Agarwal Vinayak Kulkarni Niranjan Sahoo |
| author_facet | Soumya Ranjan Nanda Sumit Agarwal Vinayak Kulkarni Niranjan Sahoo |
| author_sort | Soumya Ranjan Nanda |
| collection | DOAJ |
| description | 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. |
| format | Article |
| id | doaj-art-0d911785ad764b47a857ee1f97f55356 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2017-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-0d911785ad764b47a857ee1f97f553562025-02-03T01:00:38ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742017-01-01201710.1155/2017/20104762010476Shock Tube as an Impulsive Application DeviceSoumya Ranjan Nanda0Sumit Agarwal1Vinayak Kulkarni2Niranjan Sahoo3Department of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati 781 039, IndiaDepartment of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati 781 039, IndiaDepartment of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati 781 039, IndiaDepartment of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati 781 039, IndiaCurrent 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.http://dx.doi.org/10.1155/2017/2010476 |
| spellingShingle | Soumya Ranjan Nanda Sumit Agarwal Vinayak Kulkarni Niranjan Sahoo Shock Tube as an Impulsive Application Device International Journal of Aerospace Engineering |
| title | Shock Tube as an Impulsive Application Device |
| title_full | Shock Tube as an Impulsive Application Device |
| title_fullStr | Shock Tube as an Impulsive Application Device |
| title_full_unstemmed | Shock Tube as an Impulsive Application Device |
| title_short | Shock Tube as an Impulsive Application Device |
| title_sort | shock tube as an impulsive application device |
| url | http://dx.doi.org/10.1155/2017/2010476 |
| work_keys_str_mv | AT soumyaranjannanda shocktubeasanimpulsiveapplicationdevice AT sumitagarwal shocktubeasanimpulsiveapplicationdevice AT vinayakkulkarni shocktubeasanimpulsiveapplicationdevice AT niranjansahoo shocktubeasanimpulsiveapplicationdevice |