Zobrazeno 1 - 10
of 33
pro vyhledávání: '"William R. Lindberg"'
Publikováno v:
Sensors, Vol 8, Iss 4, Pp 2707-2721 (2008)
This paper discusses a novel dynamic resonant wall shear stress sensor concept based on an oscillating sensor operating near resonance. The interaction between the oscillating sensor surface and the fluid above it is modelled using the unsteady lamin
Externí odkaz:
https://doaj.org/article/b74582dab2a14bd1be7320c89c6c7c28
Publikováno v:
Experiments in Fluids. 53:1107-1121
Experimental measurements are used to validate a numerical model of a dynamic resonant wall shear stress sensor. The numerical model consists of an unsteady two-dimensional boundary-layer model for the flow and a simple mechanical model for the senso
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::00a5e0807cb3d370aaeeae137be92420
https://doi.org/10.1007/s00348-012-1347-8
https://doi.org/10.1007/s00348-012-1347-8
Publikováno v:
Computers & Fluids. 38:340-346
Despite the importance of wall shear stress measurements in both fundamental and applied fluid dynamic problems, sensors for this application suffer from several shortcomings. A new class of wall shear stress sensor concept that addresses these short
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44504545c9f3736d5e2ff73db005dc5a
https://doi.org/10.1016/j.compfluid.2008.04.007
https://doi.org/10.1016/j.compfluid.2008.04.007
Publikováno v:
Sensors (Basel, Switzerland)
Sensors, Vol 8, Iss 4, Pp 2707-2721 (2008)
Sensors
Volume 8
Issue 4
Pages: 2707-2721
Sensors, Vol 8, Iss 4, Pp 2707-2721 (2008)
Sensors
Volume 8
Issue 4
Pages: 2707-2721
This paper discusses a novel dynamic resonant wall shear stress sensor concept based on an oscillating sensor operating near resonance. The interaction between the oscillating sensor surface and the fluid above it is modelled using the unsteady lamin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::dedcf5334d1b0005f7798276598ddff9
https://doi.org/10.3390/s8042707
https://doi.org/10.3390/s8042707
Publikováno v:
Journal of Fluids Engineering. 125:275-282
Impulsively started impinging jets were experimentally investigated in a water tank utilizing a fluorescent dye technique. The jets were examined prior to and subsequent to impingement. The impingement surfaces included a flat surface and a two-dimen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f244f510475f06c0007dd57be21c3433
https://doi.org/10.1115/1.1537255
https://doi.org/10.1115/1.1537255
Publikováno v:
Journal of Aircraft. 35:905-911
Wind-tunnel tests were conducted to determine the performance degradation of a scaled two-dimensional NACA 23012 airfoil (outboard wing section of the Wyoming King Air 200T ) resulting from 1 ) ice because of various liquid hydrometeor sizes, 2 ) sim
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::318787cdee8272fd90c812055a3862b1
https://doi.org/10.2514/2.2385
https://doi.org/10.2514/2.2385
Publikováno v:
Journal of Aircraft. 33:1040-1046
A wind-tunnel test was conducted to determine the performance degradation of a scaled two-dimensional NAC A 23012 airfoil (outboard wing section of the Wyoming King Air 200T) resulting from various liquid hydrometeor sizes. The hydrometeor sizes cons
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b0e5a50bc05571b856ff37c5f199b77c
https://doi.org/10.2514/3.47055
https://doi.org/10.2514/3.47055
Publikováno v:
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.
Flow fleld behind an oscillating fence has been studied using phase-locked Particle Image Velocimetry. Measurements were conducted in the Strouhal number range Sta = 0.008 0.2 along the mid-span of the fence to develop an understanding of the efiect
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::90fee97b87096f8e5f541a1ac7750963
https://doi.org/10.2514/6.2010-91
https://doi.org/10.2514/6.2010-91
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b150539a2c6c5de7be9df62b20e5c6fb
https://doi.org/10.2514/6.2008-1337
https://doi.org/10.2514/6.2008-1337
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Experiments have been conducted to characterize the ability of a fence actuator to alter the aerodynamic loading of stationary and pitch oscillating wings. In particular, an oscillating fence on a NACA-23012 airfoil has been examined using Particle I
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0f9045d7160545e4a4e9f29b8f2d644b
https://doi.org/10.2514/6.2008-280
https://doi.org/10.2514/6.2008-280