| contributor author | Jiankun Yuan | |
| contributor author | David J. Olinger | |
| date accessioned | 2017-05-08T21:16:12Z | |
| date available | 2017-05-08T21:16:12Z | |
| date copyright | April 2005 | |
| date issued | 2005 | |
| identifier other | %28asce%290893-1321%282005%2918%3A2%28111%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/45024 | |
| description abstract | Deficiencies exist in our current ability to measure lift forces in wind-tunnel experiments on vibrating structures in a fluid flow. The ultrasonic lift measurement (ULM) technique has been previously developed to measure time-averaged fluid circulation and lift on stationary structures. The ULM technique is based on measuring transit times of acoustic pulses along paths enclosing the structure. A quasi-steady method based on the Kutta–Joukowski theorem has been used in the past to convert fluid circulation to lift values in ULM studies. In this paper, the largely unstudied extension of the ULM technique to measure unsteady lift forces in flows involving structural vibration is considered. Analytic methods are developed that can be used to properly convert the instantaneous circulation measurements (attainable from ULM experiments) to lift values. These unsteady methods are validated by using numerical simulations of flows over flat plates undergoing oscillating motion. It is shown that the addition of unsteady terms provides a method with improved accuracy over the previous quasi-steady assumption. The methods are also applied to ULM data from an oscillating airfoil experiment in a preliminary study. | |
| publisher | American Society of Civil Engineers | |
| title | Ultrasonic Lift Measurement Technique for Flow-Induced Structural Vibrations | |
| type | Journal Paper | |
| journal volume | 18 | |
| journal issue | 2 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2005)18:2(111) | |
| tree | Journal of Aerospace Engineering:;2005:;Volume ( 018 ):;issue: 002 | |
| contenttype | Fulltext | |