A winged aerothermodynamic experimental reentry vehicle is proposed in order to verify and validate the methods of numerical aerothermodynamics as design tool additional to the classical tools, i.e., the wind tunnel. Experimental hypersonic vehicles are reviewed and the aerothermodynamic characteristic of reentry vehicles and the ground simulation problems are considered. The possible configuration and trajectory of a winged experimental vehicle are discussed, together with the required and possible measurements, and the data management and recovery. Use of the obtained data base in the establishment of the methods of numerical aerothermodynamics as additional design tool is outlined.
Acquisition of an Aerothermodynamic Data Base by Means of a Winged Experimental Reentry Vehicle
1991
40 pages
Report
Keine Angabe
Englisch
Aerothermodynamic Reentry Flight Experiments Expert
British Library Conference Proceedings | 2007
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