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D1.12: Initial Morphing Concept CFD Polars

Gardner, Anthony D. and Abdelmoula, Amine and van der Wall, Berend G. and Woods, Benjamin K.S. (2018) D1.12: Initial Morphing Concept CFD Polars. Project Report. Project No. 723491 – SABRE – H2020-MG-2016-2017. 27 S.

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This document presents the work done on generating initial aerodynamic data sets of the different morphing concepts for use in the comprehensive rotor analysis work. This work was split between three partners and focused on the morphing concepts which are expected to cause significant change to the cross-sectional shape of the rotor blade, namely the chord extension and camber change concepts. The methodology behind the analysis done is presented, followed by the results obtained.

Item URL in elib:https://elib.dlr.de/127868/
Document Type:Monograph (Project Report)
Additional Information:EU project SABRE internal report with embargoed access
Title:D1.12: Initial Morphing Concept CFD Polars
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Gardner, Anthony D.UNSPECIFIEDhttps://orcid.org/0000-0002-1176-3447UNSPECIFIED
van der Wall, Berend G.UNSPECIFIEDhttps://orcid.org/0000-0001-6144-0921UNSPECIFIED
Woods, Benjamin K.S.University of BristolUNSPECIFIEDUNSPECIFIED
Date:January 2018
Refereed publication:No
Open Access:No
Number of Pages:27
Series Name:SABRE - Shape Adaptive Blades for Rotorcraft Efficiency
Keywords:rotor, helicopter, blade, optimization, polar, chord extension, DLR-TAU
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Virtual Aerodynamic Rotorcraft (old)
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Helicopter, GO
Institute of Flight Systems > Rotorcraft
Deposited By: Winkels, Elisabeth
Deposited On:21 Jun 2019 14:54
Last Modified:20 Jun 2021 15:52

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