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An Advanced Panel Method for Compressible Subsonic Unsteady Flow Past Complex Geometries

Fiddes, Steven P. and Burkett, Chris W. and Kier, Thiemo (2015) An Advanced Panel Method for Compressible Subsonic Unsteady Flow Past Complex Geometries. International Forum on Aeroelasticity and Structural Dynamics, 28. Jun. - 02. Jul. 2015, St. Petersburg, Russische Föderation.

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This paper describes the development of a new boundary-element method for predicting the unsteady compressible flow past general configurations in subsonic flow. It permits the actual geometry of the configuration to be represented and computes the coupling between the steady and unsteady flow components. It adopts a description of the unsteady deformation of the geometry that avoids many of the limitations inherent with vortex- and doublet-lattice methods. The paper describes the issues that have been addressed in developing the method and, through 2D and 3D validation cases, demonstrates advantages over some established methods.

Item URL in elib:https://elib.dlr.de/97805/
Document Type:Conference or Workshop Item (Speech)
Title:An Advanced Panel Method for Compressible Subsonic Unsteady Flow Past Complex Geometries
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Fiddes, Steven P.Flow Solutions LimitedUNSPECIFIED
Burkett, Chris W.Flow Solutions LimitedUNSPECIFIED
Kier, ThiemoThiemo.Kier (at) DLR.deUNSPECIFIED
Date:June 2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Unsteady 3D Panel Method
Event Title:International Forum on Aeroelasticity and Structural Dynamics
Event Location:St. Petersburg, Russische Föderation
Event Type:international Conference
Event Dates:28. Jun. - 02. Jul. 2015
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 - Systems and Cabin (old)
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control > Aircraft System Dynamics
Deposited By: Kier, Thiemo
Deposited On:24 Aug 2015 15:59
Last Modified:19 Sep 2016 13:17

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