Zobrazeno 1 - 10
of 16
pro vyhledávání: '"coanda flap"'
Publikováno v:
Aerospace, Vol 7, Iss 3, p 29 (2020)
The focus of the work is on the evaluation, development and integration of a robust actuator system for three-dimensional flow control of a blown Coanda flap to improve the high lift system of commercial aircraft. As part of the research work present
Externí odkaz:
https://doaj.org/article/6e1ac7824df34dae8ce1a939ebdbc560
Publikováno v:
Aerospace, Vol 7, Iss 3, p 29 (2020)
Aerospace 2020, 7 (3), 29; https://doi.org/10.3390/aerospace7030029--https://www.mdpi.com/journal/aerospace--http://www.bibliothek.uni-regensburg.de/ezeit/?2756091--2226-4310
Aerospace 2020, 7 (3), 29; https://doi.org/10.3390/aerospace7030029--https://www.mdpi.com/journal/aerospace--http://www.bibliothek.uni-regensburg.de/ezeit/?2756091--2226-4310
The focus of the work is on the evaluation, development and integration of a robust actuator system for three-dimensional flow control of a blown Coanda flap to improve the high lift system of commercial aircraft. As part of the research work present
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::ac8e8a38bf97373f7e818294c83b5c35
https://www.mdpi.com/2226-4310/7/3/29
https://www.mdpi.com/2226-4310/7/3/29
Autor:
Roland Ewert, Pradeep Kumar, Michaela Herr, Jan Werner Delfs, Karl-Stéphane Rossignol, Alexandre Suryadi, Lennart Rossian
With the advances in reduction of propulsion related noise from aircraft, airframe noise gets more and more into focus. During approach and landing, the high-lift system of the wings becomes one major acoustic source region contributing to the overal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ac590ef6ecbf917de967f92c05cd8f13
https://doi.org/10.2514/6.2018-3139
https://doi.org/10.2514/6.2018-3139
Publikováno v:
READ 2016: Warsaw, Poland
READ 2016
READ 2016
An innovative aircraft design of the Collaborative Research Centre (SFB) 880 features a new active high-lift system. This high-lift system is comprised of a droop-nose leading edge device and a Coanda flap as the trailing edge device. It offers very
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::af249b6502a345bb38e91b9a2d07aee5
https://elib.dlr.de/104311/
https://elib.dlr.de/104311/
An innovative aircraft design of the Collaborative Research Centre (SFB) 880 features a new active high-lift system. This high-lift system is comprised of a droop-nose leading edge device and a Coanda flap as the trailing edge device. It offers very
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dris___00893::2f54cccbb4bed585150e213e60694fa0
http://resolver.tudelft.nl/uuid:0d8665b5-f40a-4682-8ed9-f9be8b02e9b7
http://resolver.tudelft.nl/uuid:0d8665b5-f40a-4682-8ed9-f9be8b02e9b7
Akademický článek
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Autor:
Jobst Henning Diekmann
This paper outlines recent flight dynamic analysis results of a civil aircraft with active high-lift system using blown Coanda flaps. The main focus lies in the trim analysis of the aircraft. Therefore, the basic structure and core elements of the no
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a65f9cfc73f15ca0c89f661e765b6bc7
https://doi.org/10.1007/s13272-014-0132-1
https://doi.org/10.1007/s13272-014-0132-1
Akademický článek
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Akademický článek
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