| contributor author | Vinayak Kulkarni | |
| contributor author | K. P. J. Reddy | |
| date accessioned | 2017-05-08T21:33:40Z | |
| date available | 2017-05-08T21:33:40Z | |
| date copyright | October 2010 | |
| date issued | 2010 | |
| identifier other | %28asce%29as%2E1943-5525%2E0000040.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56179 | |
| description abstract | A single component accelerometer-based force balance is developed, calibrated, and used for high enthalpy applications. Functionality of this force balance, for such applications, is demonstrated for the first time during high enthalpy tests in a newly established free piston- driven shock tunnel, HST3, using a 60° apex angle blunt cone model at 0° angle of incidence. Usefulness of this force balance is also confirmed, for much complicated high enthalpy flow situations, during the drag reduction studies with counterflow supersonic jet from the stagnation point. | |
| publisher | American Society of Civil Engineers | |
| title | Accelerometer-Based Force Balance for High Enthalpy Facilities | |
| type | Journal Paper | |
| journal volume | 23 | |
| journal issue | 4 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000040 | |
| tree | Journal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 004 | |
| contenttype | Fulltext | |
