Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Luis Garcillan"'
Publikováno v:
Flow, Turbulence and Combustion. 78:283-307
Despite the proven capability of synthetic-jet actuators in delaying boundary-layer separation in laboratory experiments, a capability that allows the geometry and operating conditions of these devices to be designed and selected for maximum flow-con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e354679d0d80a1df34b624dd4049337e
https://doi.org/10.1007/s10494-006-9064-0
https://doi.org/10.1007/s10494-006-9064-0
Publikováno v:
Flow, Turbulence and Combustion. 78:309-329
Due to the large parameter space that is involved in the design of synthetic-jet actuators used for flow separation control, it is essential to develop low-dimensional models for actuator-performance prediction and establish the conditions for design
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f64bed80b60b08c2616661b8ae298f30
https://doi.org/10.1007/s10494-006-9061-3
https://doi.org/10.1007/s10494-006-9061-3
Publikováno v:
The Aeronautical Journal. 109:147-155
Dye visualisation of both inclined synthetic jets and skewed synthetic jets was undertaken in a cross-flow experiment and the results were compared with those of normal synthetic jets. The process of vortex roll-up near the orifice exit and how the s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f32773477edeffeab74da68f5fe4155
https://doi.org/10.1017/s0001924000000658
https://doi.org/10.1017/s0001924000000658
Publikováno v:
Scopus-Elsevier
1 , the velocity ratio between the freestream and the exit peak velocity of the jet was set to 1.2, the Strouhal number to 0.069 and the boundary layer thickness was measured to be 9 times the diameter of the orifice. Differences in the roll-up proce
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::47d529e2f360015da18407a1e9377e7e
https://doi.org/10.2514/6.2006-318
https://doi.org/10.2514/6.2006-318
Publikováno v:
2nd AIAA Flow Control Conference.
*† ‡ § PIV measurements have been undertaken on synthetic jets with rectangular orifices of different aspect ratios and circular orifices of different inclination angles in quiescent conditions. The results were compared with those from normal c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bc8605f8b7f2f372378ae655b3ecaa17
https://doi.org/10.2514/6.2004-2213
https://doi.org/10.2514/6.2004-2213