Abstract
This paper describes the direct coupling of missile DATCOM and the Euler/Navier-Stokes solver DLR-TAU code to the trajectory optimization program REENT-6D. The coupling of computational codes is applied along the SHarp Edge Flight EXperiment (SHEFEX I) ascent trajectory. Firstly, results of a three and six degree-of-freedom coupling between REENT-6D and DATCOMare compared with flight data. In a second step, the roll behavior of the second stage is analyzed with the DLR-TAU code including the rigid body motion. The main objectives are the application of the recent developed numerical methods and the comparison of the obtained results with flight data as a first step to rebuild the SHEFEX I flight.
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© 2013 Springer-Verlag Berlin Heidelberg
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Bartolomé Calvo, J., Wolkow, S., Eggers, T. (2013). Application of a Coupling of Flight Mechanics and Aerodynamics to Predict the SHEFEX I Ascent Phase. In: Dillmann, A., Heller, G., Kreplin, HP., Nitsche, W., Peltzer, I. (eds) New Results in Numerical and Experimental Fluid Mechanics VIII. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 121. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-35680-3_9
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DOI: https://doi.org/10.1007/978-3-642-35680-3_9
Publisher Name: Springer, Berlin, Heidelberg
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