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- W2005093265 abstract "Ground based testing of the HyShot II supersonic combustion ramjet flight configurationwas carried out in the High Enthalpy Shock Tunnel Gottingen, HEG, of the GermanAerospace Center, DLR. The main focus of these investigations was to obtain surfacepressure and surface heat transfer data on the intake and the cowl and body side surfaces ofthe combustion chamber and the nozzle. Further, high speed flow visualisation of thecombustor flow was performed. Two HEG operating conditions which are related to 33kmand 27km flight altitude were applied. Computational fluid dynamics (CFD) was applied tosupport the analysis of the experimental results and for the prediction of the free streamconditions in the HEG test section." @default.
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- W2005093265 date "2008-04-28" @default.
- W2005093265 modified "2023-09-25" @default.
- W2005093265 title "Ground Testing of the HyShot II Scramjet Configuration in HEG" @default.
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- W2005093265 doi "https://doi.org/10.2514/6.2008-2547" @default.
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