Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Maayan, Possti"'
Publikováno v:
AIAA Journal. 60:3671-3681
An experimental study on the application of active flow control (AFC) to a 1:8.4 scale model of a swept wing in a landing configuration was conducted. The wing is fitted with an Ultra High Bypass Ratio (UHBR) engine nacelle. The highly efficient UHBR
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=sygma_______::0ce019302ce1624f844e421707ec5c4b
https://doi.org/10.5281/zenodo.4288403
https://doi.org/10.5281/zenodo.4288403
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783030252526
Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Notes on Numerical Fluid Mechanics and Multidisciplinary Design-New Results in Numerical and Experimental Fluid Mechanics XII
New Results in Numerical and Experimental Fluid Mechanics XII-Contributions to the 21st STAB/DGLR Symposium, Darmstadt, Germany, 2018
Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Notes on Numerical Fluid Mechanics and Multidisciplinary Design-New Results in Numerical and Experimental Fluid Mechanics XII
New Results in Numerical and Experimental Fluid Mechanics XII-Contributions to the 21st STAB/DGLR Symposium, Darmstadt, Germany, 2018
Simulations of near zero pressure gradient turbulent boundary layer interacting with Suction and Oscillatory Blowing (SaOB) were conducted using URANS equations. Different blowing velocity Boundary Conditions (BC) and spatial resolutions were investi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7b19283aba239e149bc092a4cff71274
https://doi.org/10.1007/978-3-030-25253-3_60
https://doi.org/10.1007/978-3-030-25253-3_60
An experimental study on the application of active flow control (AFC) to a 1:8.4 scale model of a swept wing in a landing configuration was conducted. The wing is fitted with an Ultra High Bypass Ratio (UHBR) engine nacelle. The highly efficient UHBR
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0ce019302ce1624f844e421707ec5c4b
An experimental study on the application of active flow control (AFC) to a 1:8.4 scale model of a swept wing in a landing configuration was conducted. The wing is fitted with an Ultra High Bypass Ratio (UHBR) engine nacelle. The highly efficient UHBR
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1ce99e1af327d30b0bcb8e021e48777d