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High-lift design for a forward swept natural laminar flow wing

Keller, Dennis (2019) High-lift design for a forward swept natural laminar flow wing. CEAS Aeronautical Journal, 11, pp. 81-92. Springer. doi: 10.1007/s13272-019-00396-z. ISSN 1869-5590.

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Official URL: https://doi.org/10.1007/s13272-019-00396-z


The scope of the paper is to present the results of a RANS-based aerodynamic high-lift design for a natural laminar flow wing with negative sweep. The chosen high-lift system consists of a Krueger leading edge flap with shielding function and a fixed-vane trailing edge flap. The design was first optimized in two main wing sections and then verified by 3D RANS simulations of a wing-body model. Finally, engines were added to the geometric model to estimate the high-lift performance of the landing configuration. With a maximum lift coefficient of C_L,max=2.85 for the wing-body model with engine, the target from the preliminary aircraft design was reached. Further potential for improvement was found in the optimization strategy and the shape of the fuselage--wing junction.

Item URL in elib:https://elib.dlr.de/131288/
Document Type:Article
Title:High-lift design for a forward swept natural laminar flow wing
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Keller, DennisUNSPECIFIEDhttps://orcid.org/0000-0002-1471-9433UNSPECIFIED
Date:11 May 2019
Journal or Publication Title:CEAS Aeronautical Journal
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Page Range:pp. 81-92
EditorsEmailEditor's ORCID iDORCID Put Code
Keywords:Aerodynamics, High-Lift, Laminar Flow, RANS
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation (old)
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Keller, Dennis
Deposited On:06 Dec 2019 10:00
Last Modified:05 Nov 2020 15:28

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