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CFD study on a missile in pitching motion with respect of reducing the Phantom Yaw Effect

Schnepf, Christian and Schülein, Erich (2016) CFD study on a missile in pitching motion with respect of reducing the Phantom Yaw Effect. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer International Publishing Switzerland. pp. 833-842. ISBN 978-3-319-27278-8. ISSN 1612-2909

Full text not available from this repository.

Official URL: http://link.springer.com/book/10.1007/978-3-319-27279-5/page/2

Abstract

This numerical study is about the alleviation of the Phantom Yaw Effect on a pitching missile. A pair of slit shaped side jets, so called aerostrakes is used to force a symmetric separation at the shoulder of the missile. The unsteady Reynolds averaged Navier-Stokes equation are solved with a two equation turbulence model for a case with and without applied aerostrakes. The missile is pitching sinusoidally at a frequency of 5 Hz between 0° ≤ α ≤ 44 °at Mach 0.8. The results Show that the magnitude of the side force, resulting from Phantom Yaw, is reduced by the aerostrakes and the onset angle for the PYE is shifted to higher angle of attack. A reversal of sign of both the side force an yawing monemt is also prevented when using the aerostrakes. Furthermore, the influence of the pitching motion on the relevant aerodynamic coefficients is less profound in the case with aerostrakes.

Item URL in elib:https://elib.dlr.de/93333/
Document Type:Contribution to a Collection
Additional Information:ISBN: 978-3-319-27278-8 (Print) 978-3-319-27279-5 (Online)
Title:CFD study on a missile in pitching motion with respect of reducing the Phantom Yaw Effect
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schnepf, Christianchristian.schnepf (at) dlr.deUNSPECIFIED
Schülein, Ericherich.schuelein (at) dlr.deUNSPECIFIED
Date:January 2016
Journal or Publication Title:New Results in Numerical and Experimental Fluid Mechanics X
Refereed publication:Yes
Open Access:No
In DOAJ:No
In SCOPUS:No
In ISI Web of Science:No
Volume:132
DOI :10.1007/978-3-319-27279-5_73
Page Range:pp. 833-842
Editors:
EditorsEmail
Dillmann, AndreasDLR Göttingen
Heller, GerdAirbus Deutschland, Bremen, Germany
Krämer, EwaldUNI Stuttgart
Wagner, ClausDLR Göttingen
Breitsamer, ChristianTU München
Publisher:Springer International Publishing Switzerland
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-319-27278-8
Status:Published
Keywords:Phantom Yaw, Vortex asymmetry, Pitching slender body
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: Bachmann, Barbara
Deposited On:11 Jul 2016 09:29
Last Modified:22 Jan 2018 16:50

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