Design Study of a Two-Parted Variable Inlet Guide Vane with an Optimized Axial Gap

Gouezou, William and Hemmert-Pottmann, Stefan and Nicke, Eberhard (2017) Design Study of a Two-Parted Variable Inlet Guide Vane with an Optimized Axial Gap. Deutscher Luft- und Raumfahrtkongress, 2017-09-05 - 2017-09-07, Munich, Germany.

PDF
2MB

Item URL in elib:

https://elib.dlr.de/115570/

Document Type:

Conference or Workshop Item (Lecture)

Title:

Design Study of a Two-Parted Variable Inlet Guide Vane with an Optimized Axial Gap

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Gouezou, William	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Hemmert-Pottmann, Stefan	UNSPECIFIED	https://orcid.org/0000-0003-1397-750X	UNSPECIFIED
Nicke, Eberhard	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

7 September 2017

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

axial compressor, design optimization, variable inlet guide vane

Event Title:

Deutscher Luft- und Raumfahrtkongress

Event Location:

Munich, Germany

Event Type:

national Conference

Event Start Date:

5 September 2017

Event End Date:

7 September 2017

Organizer:

Deutsche Gesellschaft für Luft- und Raumfahrt

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 (old)

Location:

Köln-Porz

Institutes and Institutions:

Institute of Propulsion Technology > Fan and Compressor

Deposited By:

Pottmann, Stefan

Deposited On:

21 Nov 2017 10:08

Last Modified:

03 Mar 2026 14:13

Repository Staff Only: item control page