Compressor Leading Edge Sensitivities and Analysis with an Adjoint Flow Solver

Giebmanns, Angela and Backhaus, Jan and Frey, Christian and Schnell, Rainer (2013) Compressor Leading Edge Sensitivities and Analysis with an Adjoint Flow Solver. In: ASME Turbo Expo. ASME Turbo Expo 2013, 3.-7. Juni 2012, San Antonio, USA. doi: 10.1115/GT2013-94427.

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/83220/

Document Type:

Conference or Workshop Item (Speech, Paper)

Title:

Compressor Leading Edge Sensitivities and Analysis with an Adjoint Flow Solver

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Giebmanns, Angela	DLR-AT	UNSPECIFIED	UNSPECIFIED
Backhaus, Jan	DLR-AT	UNSPECIFIED	UNSPECIFIED
Frey, Christian	DLR-AT	UNSPECIFIED	UNSPECIFIED
Schnell, Rainer	DLR-AT	UNSPECIFIED	UNSPECIFIED

Date:

June 2013

Journal or Publication Title:

ASME Turbo Expo

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Yes

DOI:

10.1115/GT2013-94427

Status:

Published

Keywords:

Schaufelgeometrie Sensitivitäten Adjungierter Strömungslöser Simulation Optimierung

Event Title:

ASME Turbo Expo 2013

Event Location:

San Antonio, USA

Event Type:

international Conference

Event Dates:

3.-7. Juni 2012

Organizer:

ASME

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

Propulsion Systems (old)

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:

Giebmanns, Angela

Deposited On:

03 Jul 2013 13:22

Last Modified:

21 Jul 2023 08:22

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