Numerical Simulation of Maneuvering Combat Aircraft

Andreas Schütte, Gunnar Einarsson, Britta Schöning, Axel Raichle, Wulf Mönnich, Thomas Alrutz, Jens Neumann and Jörg Heinecke
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Andreas Schütte: Institute of Aerodynamics and Flow Technology, DLR
Gunnar Einarsson: Institute of Aerodynamics and Flow Technology, DLR
Britta Schöning: Institute of Aerodynamics and Flow Technology, DLR
Axel Raichle: Institute of Aerodynamics and Flow Technology, DLR
Wulf Mönnich: Institute of Flight Systems, DLR
Thomas Alrutz: Institute of Aerodynamics and Flow Technology, DLR
Jens Neumann: Institute of Aeroelasticity, DLR
Jörg Heinecke: Simulation and Software Technology, DLR

A chapter in High Performance Computing in Science and Engineering’ 05, 2006, pp 185-196 from Springer

Abstract: Summary An overview about recent results of the DLR-Project SikMa-“Simulation of Complex Maneuvers” is presented. The objective of the SikMa-Project is to develop a numerical tool to simulate the unsteady aerodynamics of a free flying aeroelastic combat aircraft, by use of coupled aerodynamic, flight-mechanic and aeroelastic computations. To achieve this objective, the unstructured, time accurate flow-solver TAU is coupled with a computational module solving the flight-mechanic equations of motion and a structural mechanics code determining the structural deformations. By use of an overlapping grid technique (chimera), simulations of a complex configuration with movable control-surfaces is possible.

Keywords: Couple Simulation; Delta Wing; Pressure Sensitive Paint; Unsteady Aerodynamic; Complex Maneuver (search for similar items in EconPapers)
Date: 2006
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Persistent link: https://EconPapers.repec.org/RePEc:spr:sprchp:978-3-540-29064-3_14

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DOI: 10.1007/3-540-29064-8_14

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