Thormann, Reik and Dimitrov, Diliana (2014) Correction of aerodynamic influence matrices for transonic flow. CEAS Aeronautical Journal. Springer. DOI: 10.1007/s13272-014-0114-3. ISSN 1869-5590.
Full text not available from this repository.
The authors present a novel correction approach for the doublet-lattice method in this paper. The doublet-lattice method is a standard tool for calculating unsteady aerodynamic loads in aeroelasticity. It solves the linear potential equations and is thus valid only at subsonic flow conditions. Hence, corrections have to be applied for transonic flow. The proposed correction method, CREAM (CorREction of Aerodynamic Matrices), uses surface pressure distributions obtained using computational fluid dynamics (CFD) simulations for the correction. It is based on a Taylor expansion of the aerodynamic influence coefficient matrix, where the Taylor coefficients are corrected successively. The approach can be applied to quasi-steady as well as to unsteady aerodynamic calculations. The method is demonstrated on the AGARD LANN wing at transonic attached flow conditions and compared to linearized unsteady CFD computations. Two different correction orders are examined: a ‘‘zeroth order correction’’ with a quasi-steady CFD sample as correction input and a ‘‘first order correction’’ with an additional unsteady CFD sample. It is shown that CREAM gives improved results for small reduced frequencies, where the first-order correction is always superior to the zeroth order correction.
|Title:||Correction of aerodynamic influence matrices for transonic flow|
|Journal or Publication Title:||CEAS Aeronautical Journal|
|In Open Access:||No|
|In ISI Web of Science:||No|
|Keywords:||AIC, DLM Correction, CFD, Transonic flow, Unsteady flow|
|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 - Simulation and Validation|
|Institutes and Institutions:||Institute of Aeroelasticity > Aeroelastic Simulations|
|Deposited By:||Reik Thormann|
|Deposited On:||07 Aug 2014 13:37|
|Last Modified:||29 Jun 2015 03:04|
Repository Staff Only: item control page