Sounding Rockets as a Real Flight Platform for Aerothermodynamic CFD Validation of Hypersonic Experiments
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This paper describes the possibilities of sounding rockets to provide a platform for flight experiments in hypersonic conditions as a supplement to wind tunnel tests. Real flight data from measurement durations longer than 30 seconds can be compared with predictions from CFD calculations. This paper will regard projects flown on sounding rockets, but mainly describe the current efforts at Mobile Rocket Base, DLR on the SHarp Edge Flight EXperiment SHEFEX.
[1] J.M.A. Longo,et al. The sharp edge flight experiment SHEFEX , 2002 .
[2] Johan Steelant,et al. Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG and Comparison with Flight Data (AIAA 2004–3345) , 2004 .
[3] Arthur E. Bryson,et al. Control of spacecraft and aircraft , 1994 .