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Deliverable D1.2, part II: Report on Analytical Adaptive Rotor Studies: Synthesis of the Baseline NACA 23012tab Airfoil

van der Wall, Berend G. (2018) Deliverable D1.2, part II: Report on Analytical Adaptive Rotor Studies: Synthesis of the Baseline NACA 23012tab Airfoil. Project Report. 26 S.

Full text not available from this repository.

Abstract

This report is about the synthesis of the baseline NACA 23012tab airfoil coefficients computed within Task 1.4 by DLR-AS. The theory of the analytical model is outlined and its coefficients identified using those data. Comparison with the data is provided.

Item URL in elib:https://elib.dlr.de/118947/
Document Type:Monograph (Project Report)
Additional Information:EU project SABRE internal report with embargoed access.
Title:Deliverable D1.2, part II: Report on Analytical Adaptive Rotor Studies: Synthesis of the Baseline NACA 23012tab Airfoil
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
van der Wall, Berend G.UNSPECIFIEDhttps://orcid.org/0000-0001-6144-0921UNSPECIFIED
Date:6 February 2018
Refereed publication:No
Open Access:No
Number of Pages:26
Status:Published
Keywords:SABRE, Shape Adaptive Blades for Rotorcraft Efficiency, semi-empirical modeling, airfoil coefficient simulation
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 (old)
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:15 Feb 2018 15:22
Last Modified:20 Jun 2021 15:50

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