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Numerical investigation on the Phantom Yaw Effect induced due to small nose deflection

Schnepf, Christian and Wysocki, Oliver and Schülein, Erich (2013) Numerical investigation on the Phantom Yaw Effect induced due to small nose deflection. American Institute of Aeronautics and Astronautics. 31rd Applied Aerodynamics Conference, 24. - 27. Juni 2013, San Diego, USA.

Full text not available from this repository.

Official URL: http://arc.aiaa.org | DOI: 10.2514/6.2013-3034

Abstract

The effect of a small nose deformation on the vortex formation on a missile geometry at high angles of attack has been numerically investigated. The closure of the RANS-equation has been done with a two equation turbulence model and solved with the state of the art DLR-TAU-code. For this investigation the boundary layer is considered as fully turbulent. Using radial basis function, the forepart of the missile was deformed in the horizontal plane at different positions along the roll axis. Applying deformations with magnitudes close to measured values on a wind tunnel model, side forces were gained similar to the values of a wind tunnel experiment. Like in the mentioned experiment, the vortex asymmetry could be diminished by a pair of jet-strakes meaning the ejection of narrow side jets at the shoulder area of the body.

Item URL in elib:https://elib.dlr.de/82456/
Document Type:Conference or Workshop Item (Speech)
Additional Information:DOI: 10.2514/6.2013-3034
Title:Numerical investigation on the Phantom Yaw Effect induced due to small nose deflection
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schnepf, Christianchristian.schnepf (at) dlr.deUNSPECIFIED
Wysocki, Oliveroliver.wysocki (at) dlr.deUNSPECIFIED
Schülein, Ericherich.schuelein (at) dlr.deUNSPECIFIED
Date:2013
Refereed publication:No
Open Access:No
In DOAJ:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-22
Publisher:American Institute of Aeronautics and Astronautics
Series Name:Conference Proceedings online
Status:Published
Keywords:phantom yaw, flow control
Event Title:31rd Applied Aerodynamics Conference
Event Location:San Diego, USA
Event Type:international Conference
Event Dates:24. - 27. Juni 2013
Organizer:AIAA
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:26 Aug 2013 09:21
Last Modified:08 May 2014 23:18

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