Zobrazeno 1 - 10
of 42
pro vyhledávání: '"Krueger flap"'
Publikováno v:
International Journal of Numerical Methods for Heat & Fluid Flow, 2020, Vol. 31, Issue 2, pp. 618-628.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/HFF-09-2019-0687
Publikováno v:
International Journal of Numerical Methods for Heat & Fluid Flow. 31:618-628
Purpose Some recent effort showed that usage of Krueger flaps helps to maintain laminar flow in cruise flight. Such flaps are positioned higher relative to the chord to shield the leading edge from the insect contamination during take-off. The flap p
Autor:
Wild, Jochen, Palazzo, Salvatore, Brinza, Ionuts, van der Biest, Koen, Vervliet, Antoon, Schmitz, Holger
Publikováno v:
Advances in Computational Methods and Technologies in Aeronautics and Industry ISBN: 9783031120183
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b309ce612a4ce9a5bb1aadced2dab0a9
https://doi.org/10.1007/978-3-031-12019-0_9
https://doi.org/10.1007/978-3-031-12019-0_9
Publikováno v:
Advances in Computational Methods and Technologies in Aeronautics and Industry /Computational Methods in Applied Sciences
Computational Methods in Applied Sciences
Computational Methods in Applied Sciences-Advances in Computational Methods and Technologies in Aeronautics and Industry
Advances in Computational Methods and Technologies in Aeronautics and Industry ISBN: 9783031120183
Computational Methods in Applied Sciences
Computational Methods in Applied Sciences-Advances in Computational Methods and Technologies in Aeronautics and Industry
Advances in Computational Methods and Technologies in Aeronautics and Industry ISBN: 9783031120183
The feasibility of laminar flow control technology for future wing is bound to the development of a leading edge high-lift system that complies with the requirements on smooth surfaces to enable maintaining the laminar boundary layer flow, such as a
Publikováno v:
INCAS Bulletin, Vol 4, Iss 1, Pp 3-14 (2012)
The aim of this paper is to study the unsteady aerodynamic interaction between a Krueger flap and a three-element airfoil using the finite volume method to solve the Unsteady Reynolds-Averaged Navier-Stokes equations. For a better understanding of th
Externí odkaz:
https://doaj.org/article/9ffd0c88e4904cd697c0251b3257b0c5
Akademický článek
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Autor:
KWAK, Dongyoun, OHIRA, Keisuke
Publikováno v:
日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences. 67(5):137-142
形態: 図版あり
Physical characteristics: Original contains illustrations
資料番号: PA2020037000
Physical characteristics: Original contains illustrations
資料番号: PA2020037000
Autor:
Keisuke Ohira, Dong-Youn Kwak
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 67:137-142