Fan tone simulation from a UHBR engine with drooped nacelle inlet at Approach condition and an angle of attack of 10°

Holewa, Axel and Guerin, Sebastien (2017) Fan tone simulation from a UHBR engine with drooped nacelle inlet at Approach condition and an angle of attack of 10°. 21st Workshop of the Aeroacoustics Specialists Committee of the CEAS, 2017-09-13 - 2017-09-15, Dublin, Ireland.

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/117977/

Document Type:

Conference or Workshop Item (Speech)

Title:

Fan tone simulation from a UHBR engine with drooped nacelle inlet at Approach condition and an angle of attack of 10°

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Holewa, Axel	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Guerin, Sebastien	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

September 2017

Refereed publication:

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

acoustics, inflow distortion, mode scattering

Event Title:

21st Workshop of the Aeroacoustics Specialists Committee of the CEAS

Event Location:

Dublin, Ireland

Event Type:

Workshop

Event Start Date:

13 September 2017

Event End Date:

15 September 2017

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 - Virtual Engine and Validation methods (old)

Location:

Berlin-Charlottenburg

Institutes and Institutions:

Institute of Propulsion Technology > Engine Acoustic

Deposited By:

Guerin, Sebastien

Deposited On:

09 Jan 2018 12:03

Last Modified:

12 Jun 2024 11:47

Repository Staff Only: item control page