Zobrazeno 1 - 10
of 10
pro vyhledávání: '"AHLNS"'
Publikováno v:
AIAA SciTech Forum 2023
The Parabolized Stability Equations (PSE), Adaptive Harmonic Linearized Navier-Stokes (AHLNS) and Harmonic Navier-Stokes (HNS) solvers are used to analyze the linear and nonlinear stability of swept-wing boundary layers under the influence of smooth
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f4e5a82b651a610d1268c77a246fbc0a
https://doi.org/10.2514/6.2023-0678
https://doi.org/10.2514/6.2023-0678
Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Notes on Numerical Fluid Mechanics and Multidisciplinary Design-New Results in Numerical and Experimental Fluid Mechanics XIII
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783030795603
Notes on Numerical Fluid Mechanics and Multidisciplinary Design-New Results in Numerical and Experimental Fluid Mechanics XIII
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783030795603
Laminar-turbulent transition prediction is of practical interest in aircraft design since transition affects important aerodynamic quantities such as drag and heat transfer. Extended laminar flow on aerodynamic surfaces is an effective way of reducin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b6e9dd6188216f732beefb520c78fd5b
https://elib.dlr.de/135594/
https://elib.dlr.de/135594/
The interest in Hybrid Laminar Flow Control (HLFC) wings lies in the potential of suction for reducing the viscous drag on commercial aircraft wings by delaying laminar-turbulent transition. However, the joint between the leading edge suction panel a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::491bc39cb67062a24074469801ed82bb
Autor:
Franco, Juan, Hein, Stefan
The interest in Hybrid Laminar Flow Control (HLFC) wings lies in the potential of suction for reducing the viscous drag on commercial aircraft wings by delaying laminar-turbulent transition. However, the joint between the leading edge suction panel a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1640::360b911b985c50e51b99975a2fd4af29
https://elib.dlr.de/141523/
https://elib.dlr.de/141523/
Kniha
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Kniha
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Conference
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Publikováno v:
Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Notes on Numerical Fluid Mechanics and Multidisciplinary Design-New Results in Numerical and Experimental Fluid Mechanics XIII
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783030795603
Notes on Numerical Fluid Mechanics and Multidisciplinary Design-New Results in Numerical and Experimental Fluid Mechanics XIII
Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783030795603
Hybrid laminar flow control (HLFC) wings have captured the interest of several research projects, in particular the HLFC-WIN project [1], because of the potential of suction for reducing drag on commercial aircraft [2]. This reduction in drag is main
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6b074448212ebc22de4f139bac5d6fbd