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Numerical investigation on the development of the Phantom Yaw Effect on a maneuvering missile

Schnepf, Christian and Wysocki, Oliver and Schülein, Erich (2014) Numerical investigation on the development of the Phantom Yaw Effect on a maneuvering missile. American Institute of Aeronautics and Astronautics. AIAA Aviation and Aeronautics Forum and Exposition (AVIATION 2014), 16. – 20. June 2014, Atlanta, GA, USA.

Full text not available from this repository.

Official URL: http://arc.aiaa.org | DOI: 10.2514/6.2014-3097

Abstract

The aerodynamics of a pitching slender body at $M=0.8$ with two different pivot locations have been numerically investigated using URANS with a two equation turbulence model. Identical to an experiment a sinusoidal motion between $\alpha=0^\circ$ and $44^\circ$ was defined. Due to a deflection of the symmetric numerical grid a vortex asymmetry the so called Phantom Yaw Effect was triggered. While the lift and drag are highly dependent on the pivot the side force and the yawing moment are less sensitive to the pivot. With the help of a forced symmetric separation at the nose the Phantom Yaw Effect could be reduced and the load change at higher angles of attack could be eliminated. A comparison with experimental shows a less good agreement.

Item URL in elib:https://elib.dlr.de/89296/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA 2014-3097, 32nd AIAA Applied Aerodynamics Conference, DOI: 10.2514/6.2014-3097
Title:Numerical investigation on the development of the Phantom Yaw Effect on a maneuvering missile
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:2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-23
Publisher:American Institute of Aeronautics and Astronautics
Series Name:Conference Proceedings online
Status:Published
Keywords:Phantom Yaw Effect, unsteady aerodynamics, CFD, pitching maneuver
Event Title:AIAA Aviation and Aeronautics Forum and Exposition (AVIATION 2014)
Event Location:Atlanta, GA, USA
Event Type:international Conference
Event Dates:16. – 20. June 2014
Organizer:American Institute of Aeronautics and Astronautics
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Military Technologies
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Micknaus, Ilka
Deposited On:18 Jul 2014 10:22
Last Modified:21 Oct 2014 13:52

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