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Deliverable D1.2, part I: Report on Analytical Adaptive Rotor Studies

van der Wall, Berend G. (2017) Deliverable D1.2, part I: Report on Analytical Adaptive Rotor Studies. Project Report.

Full text not available from this repository.

Abstract

This report is about computation of the rotor performance based on the baseline rotor definition from deliverable D1.1. Rotor blade adaptive twist, chord extension and combination of both are investigated with respect to hover figure of merit and rotor thrust enhancements, relative to the baseline rotor. The report is divided into two parts. The first part makes use of textbook-like Blade element momentum theory with certain refinements explained in detail. Results are computed assuming rigid rotor blades using Excel. The second part is a repeat of these computations using DLRs S4 isolated rotor code, which employs elastic rotor blades, nonlinear aerodynamics including stall, compressibility and various rotor wake modelling tools. Especially that report will include the modified aerodynamics of the morphed airfoils that are not considered in the first part.

Item URL in elib:https://elib.dlr.de/113829/
Document Type:Monograph (Project Report)
Additional Information:EU project SABRE internal report with embargoed access.
Title:Deliverable D1.2, part I: Report on Analytical Adaptive Rotor Studies
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
van der Wall, Berend G.berend.vanderwall (at) dlr.dehttps://orcid.org/0000-0001-6144-0921
Date:September 2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:30
Status:Published
Keywords:SABRE, Shape Adaptive Blades for Rotorcraft Efficiency, Rotor blade morphing
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 Innovative Rotorcraft
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:04 Sep 2017 13:22
Last Modified:04 Sep 2017 13:22

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