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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, 16. - 21. Sept. 2012, Santa Barbara, USA.

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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
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Schnepf, Christianchristian.schnepf (at) dlr.deUNSPECIFIED
Date:September 2012
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:slender body, phantov yaw, flow control
Event Title:22nd Liepmann-Ludwieg Seminar
Event Location:Santa Barbara, USA
Event Type:Workshop
Event Dates:16. - 21. Sept. 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:22 Oct 2012 16:11

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