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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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Abstract

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
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gardner, Anthony D.anthony.gardner (at) dlr.dehttps://orcid.org/0000-0002-1176-3447
Abdelmoula, AmineTU MunichUNSPECIFIED
van der Wall, Berend G.berend.vanderwall (at) dlr.dehttps://orcid.org/0000-0001-6144-0921
Woods, Benjamin K.S.University of BristolUNSPECIFIED
Date:January 2018
Refereed publication:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:27
Series Name:SABRE - Shape Adaptive Blades for Rotorcraft Efficiency
Status:Published
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
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:21 Jun 2019 14:54

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