Flow control on slender bodies at high angle of attack

Schnepf, Christian (2012) Flow control on slender bodies at high angle of attack. 22nd Liepmann-Ludwieg Seminar, 2012-09-16 - 2012-09-21, Santa Barbara, USA.

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Abstract

In the speech the effect of a blowing jet on the flow separation of a slender body is demonstrated, The jet acts on either side of the slender body near the junction of the cylindrical part and the ogive nose part of the slender body. Also the potential of a self-aligning Spike is demonstrated. In the speech just numerical results are shown.

Item URL in elib:

https://elib.dlr.de/77544/

Document Type:

Conference or Workshop Item (Speech)

Title:

Flow control on slender bodies at high angle of attack

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Schnepf, Christian	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

September 2012

Refereed publication:

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Status:

Published

Keywords:

slender body, phantov yaw, flow control

Event Title:

22nd Liepmann-Ludwieg Seminar

Event Location:

Santa Barbara, USA

Event Type:

Workshop

Event Start Date:

16 September 2012

Event End Date:

21 September 2012

Organizer:

University of California, Santa Barbara (UCSB)

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Aeronautics

HGF - Program Themes:

Aircraft Research (old)

DLR - Research area:

Aeronautics

DLR - Program:

L AR - Aircraft Research

DLR - Research theme (Project):

L - Flight Physics (old)

Location:

Göttingen

Institutes and Institutions:

Institute of Aerodynamics and Flow Technology > High Speed Configurations

Deposited By:

Schnepf, Christian

Deposited On:

22 Oct 2012 16:11

Last Modified:

24 Apr 2024 19:43

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