Numerical Simulation of Oscillating Wing Using Linear and Nonlinear CFD Methods (CROSBI ID 524414)
Prilog sa skupa u zborniku | sažetak izlaganja sa skupa | međunarodna recenzija
Podaci o odgovornosti
Majić, Frane
engleski
Numerical Simulation of Oscillating Wing Using Linear and Nonlinear CFD Methods
The direct simulation of structure-fluid coupling in the time domain adopting the most precise modelling techniques needs extremely high computational effort. As the main effort is needed for the part of computing unsteady aerodynamic loads by RANS solvers, more efficient methods have been developed for the task of predicting only the flutter boundary. The aerodynamic part of the solution procedure then comprises the computation of unsteady aerodynamic flows around the aircraft structures performing oscillatory dynamic motions in different known elastic geometrical modes and with different frequencies. In this work this is very efficiently performed by two codes. First, the Transonic Doublet Lattice Method (TDLM) with importing of steady results from CFD code (Tau), and second by the CFD code for RANS equations (Tau). Steady results are imported into TDLM grid from unstructured grid which was not possible before. The interpolation between structured and unstructured grids was difficult and time consuming, due to the non-ordered character of the unstructured grid. For this purpose, fast interpolation method has been developed. In the work, procedure is applied to the AMP (Aeroelastisches Modellprogramm) wing, a wind tunnel model of a typical transport aircraft wing. The TDLM unsteady results are compared with Tau and experimental results.
oscillating wing; TSD equation
nije evidentirano
nije evidentirano
nije evidentirano
nije evidentirano
nije evidentirano
nije evidentirano
Podaci o prilogu
124-125-x.
2006.
objavljeno
Podaci o matičnoj publikaciji
STAB
Heinemann, Hajo
Göttingen: Deutsches Zentrum für Luft- und Raumfahrt (DLR)
Podaci o skupu
Nepoznat skup
predavanje
29.02.1904-29.02.2096