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Numerical study on the Impact of a maneuver in the Phantom-Yaw-Effect in transonic flow

Schnepf, Christian and Wysocki, Oliver and Schülein, Erich (2018) Numerical study on the Impact of a maneuver in the Phantom-Yaw-Effect in transonic flow. In: AIAA Aviation 2018. AIAA Aviation and Aeronautics Forum and Exposition 2018, 25.-29. Juni 2018, Atlanta, Georgia, USA. doi: 10.2514/6.2018-4124.

Full text not available from this repository.

Official URL: https://arc.aiaa.org/doi/abs/10.2514/6.2018-4124


The impact of a dynamic maneuver on the Phantom-Yaw-Effect has been investigated numerically using the finite volume flow solver DLR-TAU-Code. URANS-simulations have been carried out for a generic missile configuration undergoing a sinusoidal pitching motion between an angle of attack of 0° and 44° with a reduced frequency of k=0.0042 at a Mach number of M=0.8. In addition, simulations at fixed angle of attack were performed. The Phantom Yaw Effect itself was triggered due to a slight deformation of the missile. It was found that the magnitude and the angular position of the peak values of the arising side forces are significantly influenced by the maneuver. On the other hand the general development of the Phantom-Yaw-Effect as a function of angle of attack does not change fundamentally with the pitching motion, except near the upper inflection point of the sine movement. An investigation using a locally forced symmetric boundary layer separation close to the nose changed the Phantom-Yaw-Effect in a positive manner and reduced the arising side force.

Item URL in elib:https://elib.dlr.de/119027/
Document Type:Conference or Workshop Item (Speech)
Title:Numerical study on the Impact of a maneuver in the Phantom-Yaw-Effect in transonic flow
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Schnepf, ChristianChristian.Schnepf (at) dlr.deUNSPECIFIED
Wysocki, OliverRolls Royce, 15827 Blankenfelde-Mahlow, Eschenweg 11, GermanyUNSPECIFIED
Schülein, ErichErich.Schuelein (at) dlr.dehttps://orcid.org/0000-0002-1125-8504
Journal or Publication Title:AIAA Aviation 2018
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
DOI :10.2514/6.2018-4124
Keywords:Flugkörper, Experiment, Numerik, Phantom-Yaw-Effekt
Event Title:AIAA Aviation and Aeronautics Forum and Exposition 2018
Event Location:Atlanta, Georgia, USA
Event Type:international Conference
Event Dates:25.-29. Juni 2018
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 (old)
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > High Speed Configurations, GO
Deposited By: Schnepf, Christian
Deposited On:02 Nov 2018 15:07
Last Modified:02 Nov 2018 15:19

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