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TDLM - A Transonic Doublet Lattice Method for 3D Potential Unsteady Transonic Flow Calculation.

Lu, S. and Voß, R. (1992) TDLM - A Transonic Doublet Lattice Method for 3D Potential Unsteady Transonic Flow Calculation. DLR-Forschungsbericht. 92-25, 43 S.

Full text not available from this repository.

Abstract

In this report, a Transonic Doublet Lattice Method (TDLM) for calculating unsteady transonic pressure distributions and airloads isdeveloped. The flow around harmonically oscillating surfaces is described by superposition of a steady transonic mean flow and an unsteady harmonic flow. The unsteady flow component is modelled by acceleration potential doublets on the mean wing surface and a source distribution in the flow field near the wing. The time-linearized unsteady transonic small perturbation equation is solved by an integral equation method. Results for a rectangular wing, the Northrop F-5 wing, and the LANN wing in pitching oscillation are presented. Comparisons are made with both experimental and other numerical results. Agreement with the experimental results is very good. The computing time on the IBM 3090 is less than ten minutes for one reduced frequency, and it shows that the TDLM can provide a sufficiently accurate and cost-effective procedure for routine transonic flutter calculations.

Item URL in elib:https://elib.dlr.de/39534/
Document Type:Monograph (DLR-Forschungsbericht)
Additional Information: LIDO-Berichtsjahr=1992,
Title:TDLM - A Transonic Doublet Lattice Method for 3D Potential Unsteady Transonic Flow Calculation.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lu, S.Nanjing Aeronautical Institute, VR ChinaUNSPECIFIED
Voß, R.UNSPECIFIEDUNSPECIFIED
Date:1992
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:43
Status:Published
Keywords:Unsteady transonic flow, field panel method, doublet lattice method, flutter.
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:46

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