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- W205085367 abstract "Currently, the direct coupling of CFD and flight mechanics during the layout is still much too time-consuming to consider the free motion of a vehicle along a complete trajectory. Therefore, it is the goal to develop a modular coupling procedure between the trajectory optimization code REENT [1] of the Universitat Stuttgart and the DLR surface inclination method SOSE [2], which in a later step also allows the use of the DLR Euler- and Navier-Stokes code TAU. Within the present paper the coupling procedure is introduced and basic but representative examples for sounding rocket and re-entry missions are discussed to prove the feasibility of the procedure." @default.
- W205085367 created "2016-06-24" @default.
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- W205085367 date "2008-10-01" @default.
- W205085367 modified "2023-09-27" @default.
- W205085367 title "LAYOUT OF HYPERSONIC VEHICLES BY COUPLING OF AERODYNAMICS AND FLIGHTMECHANICS" @default.
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