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Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration

Rohlmann, David (2015) Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration. In: Advances in Simulation of Wing and Nacelle Stall Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), 131. Springer International Publishing. pp. 381-395. ISBN 978-3-319-21126-8. ISSN 1612-2909

Full text not available from this repository.

Official URL: http://www.springer.com/series/4629

Abstract

Within the German national research project HINVA (High-lift INflight VAlidation) the prediction of maximum lift of realistic transport aircraft configurations shall be improved. This is achieved by a close link of flight tests, cryogenic wind tunnel tests and numerical simulations. Within the HINVA flight test campaign in 2012 several so called pressure belts were installed on one wing of the Airbus A320 used for the flight tests to measure surface pressure data on the wing for the complete polar up to C_Lmax. To investigate the influence of these belts on the measured data, a numerical investigation was performed. This paper will show the results of the these investigations by a comparison of simulations with and without pressure belts.

Item URL in elib:https://elib.dlr.de/99944/
Document Type:Contribution to a Collection
Title:Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rohlmann, Daviddavid.rohlmann (at) dlr.deUNSPECIFIED
Date:2015
Journal or Publication Title:Advances in Simulation of Wing and Nacelle Stall
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:131
DOI :10.1007/978-3-319-21127-5
Page Range:pp. 381-395
Editors:
EditorsEmail
Radespiel, RolfTU Braunschweig
Niehuis, ReinhardUniversität der Bundeswehr München
Kroll, NorbertDLR Braunschweig
Behrends, KathrinTU Braunschweig
Publisher:Springer International Publishing
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM)
ISSN:1612-2909
ISBN:978-3-319-21126-8
Status:Published
Keywords:Hochauftriebsaerodynamik, CFD
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, L - Flight Physics
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Rohlmann, David
Deposited On:25 Nov 2015 12:00
Last Modified:10 May 2016 23:35

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