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A Database of Optimal Airfoils for Axial Compressor Throughflow Design

Schnoes, Markus and Nicke, Eberhard (2016) A Database of Optimal Airfoils for Axial Compressor Throughflow Design. ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition, 13.-17. Juni 2016, Seoul, Südkorea.

Full text not available from this repository.

Abstract

This text describes methods to organize a large set of optimized airfoils in a relational database and its application in throughflow design. Optimized airfoils are structured in five dimensions: inlet Mach number, blade stagger angle, pitch-chord ratio, maximum thickness-chord ratio and a parameter for aerodynamic loading. In this space, a high number of airfoil geometries is generated by means of numerical optimization. Each airfoil geometry is tailored to its specific requirements and optimized for a wide working range as well as low losses. During the optimization of each airfoil, performance in design and off-design conditions is evaluated with the blade-to-blade flow solver MISES. Together with airfoil geometry, the database stores automatically calibrated correlations which describe cascade performance in throughflow calculation. Based on these methods, two subsonic stages of a 4.5-stage transonic research compressor are redesigned. Performance of baseline and updated geometries is evaluated with 3D CFD. The overall approach offers accurate throughflow design incorporating optimized airfoil shapes and a fast transition from throughflow to 3D CFD design.

Item URL in elib:https://elib.dlr.de/111309/
Document Type:Conference or Workshop Item (Speech)
Title:A Database of Optimal Airfoils for Axial Compressor Throughflow Design
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schnoes, Markusmarkus.schnoes (at) dlr.deUNSPECIFIED
Nicke, EberhardEberhard.Nicke (at) dlr.deUNSPECIFIED
Date:June 2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Axial Compressor Design; Throughflow; Optimization; Database
Event Title:ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition
Event Location:Seoul, Südkorea
Event Type:international Conference
Event Dates:13.-17. Juni 2016
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Fan and Compressor Technologies
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Schnös, Markus
Deposited On:01 Mar 2017 11:31
Last Modified:01 Mar 2017 11:31

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