After more than 50 years, high-enthalpy facilities suitable for aerodynamic testing in the hypersonic regime are still mostly based on the shock tunnel principle. Recent use of these facilities involves the development of space planes, reentry vehicles and scramjets for studying the complex aerothermochemistry associated with these vehicles.
CITATION STYLE
Olivier, H. (2016). The aachen shock tunnel th2 with dual driver mode operation. In Experimental Methods of Shock Wave Research (pp. 111–129). Springer International Publishing. https://doi.org/10.1007/978-3-319-23745-9_5
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