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Linearised RANS solver



 Comparison of the complex transmission function between wing lift and pitch angle
zum Bild Comparison of the complex transmission function between wing lift and pitch angle

The Institute of Aeroelasticity, together with the Institute of Aerodynamics and Flow Technology, is developing the linear frequency domain (LFD) solver in TAU. On the basis of a previously determined conventional steady solution, and given a separation amplitude field, this method enables the direct calculation of a complete complex-valued interference flow field or a complex interfering pressure distribution on a surface oscillating with constant frequency. A requirement of the LFD method is that it always delivers exactly the same solution as the conventional time domain solver (TAU TD) for the special case of small interferences.

Literature:

  • Thormann, R. and Widhalm, M. (2013): Linear Frequency Do-main Prediction of Dynamic Response Data for Viscous Transonic Flows. AIAA Journal. DOI: 10.2514/1.J051896.

Contact
Dr.-Ing. David Quero Martin
Teamleader Unsteady Aerodynamics

German Aerospace Center

Institute of Aeroelasticity

Göttingen

Tel.: +49 551 709-2664

Fax: +49 551 709-2862

Related Topics
Aerodynamic
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