Search results Thormann, Reik NUK

1.	Correction of aerodynamic influence matrices for transonic flow Thormann, Reik; Dimitrov, Diliana CEAS aeronautical journal, 12/2014, Volume: 5, Issue: 4 Journal Article 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 ...	Full text
2.	Quasi-steady doublet-lattice correction for aerodynamic gust response prediction in attached and separated transonic flow Friedewald, Diliana; Thormann, Reik; Kaiser, Christoph ... CEAS aeronautical journal, 03/2018, Volume: 9, Issue: 1 Journal Article A quasi-steady doublet-lattice correction method is used to predict aerodynamic gust responses of two different configurations: a swept wing, the so-called Aerostabil wing, and a transport aircraft ...	Full text
3.	Efficient Evaluation of Dynamic Response Data with a Linearized Frequency Domain Solver at Transonic Separated Flow Condition 35th AIAA Applied Aerodynamics Conference Book Chapter Open access	Full text

Search results