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Numerical study of nonlinearity of unsteady aerodynamics for NLR7301 profile

Voß, Ralph and Saitoh, Kenichi and Kheirandish, Hamidreza (2005) Numerical study of nonlinearity of unsteady aerodynamics for NLR7301 profile. IFASD 2005 - International Forum on Aeroelasticity and Structural Dynamics, 2005-06-28 - 2005-07-01, Munich, Germany (Europe).

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Abstract

Details of unsteady aerodynamics for a two dimensional NLR7301 airfoil with flap were numerically investigated by a Navier-Stokes code in the transonic regime. Unsteady aerodynamic coefficients such as lift and pitching moment show nonlinear aspects in a small amplitude range of forced excitation modes. The pressure distribution of the supersonic region on the upper surface is very sensitive to the incidence angle, which yields the nonlinearity of the unsteady aerodynamics in a small amplitude range of pitching motion. The behaviour of reattachment of the boundary layer behind the shock wave also affects the nonlinearity. Shock wave motions were also examined. Linearized lift and pitching moment coefficients for each amplitude were applied to the Eigenvalue analysis for the flutter boundary. Time domain flutter simulations were also carried out and the result showed that the amplitude of the limit cycle oscillation could be explained by the flutter boundary of the Eigenvalue analysis.

Item URL in elib:https://elib.dlr.de/43660/
Document Type:Conference or Workshop Item (Paper)
Title:Numerical study of nonlinearity of unsteady aerodynamics for NLR7301 profile
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Voß, RalphUNSPECIFIEDUNSPECIFIED
Saitoh, KenichiJapan Aerospace Exploration Agency (JAXA)UNSPECIFIED
Kheirandish, HamidrezaResearch center of computational mechanics, Tokyo, JapanUNSPECIFIED
Date:2005
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:unsteady aerodynamics, limit cycle oscillations, transonic flutter
Event Title:IFASD 2005 - International Forum on Aeroelasticity and Structural Dynamics
Event Location:Munich, Germany (Europe)
Event Type:international Conference
Event Dates:2005-06-28 - 2005-07-01
Organizer:CEAS/AIAA/DGLR
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 - Flexible Aircraft (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: Erdmann, Daniela
Deposited On:27 Aug 2007
Last Modified:31 Jul 2019 19:17

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