Titlebook: Experimental Methods of Shock Wave Research; Ozer Igra,Friedrich Seiler Book 2016 Springer International Publishing Switzerland 2016 Exper

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Hidetaka Hamada,Mihai Iancu,Gabriela Kohrc-heated wind tunnel is one of these facilities and features long operational time; thus the arc-heated wind tunnel has been used mainly for the development and evaluation of a thermal protection system for space transportation systems. Thus generated plasma flows can be employed for the experiments

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Dorina Mitrea,Irina Mitrea,Marius Mitreaitions. Their performance range mainly depends on their driver technology which can be distinguished between conventional driver, employing pre-compressed gas, combustion and detonation driver and free piston driver. In principle, the highest performance in terms of nozzle reservoir pressure and tem

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Dorina Mitrea,Irina Mitrea,Marius Mitreaterceptors, re-entry vehicles and projectiles and to their related steering systems. The main and great advantage of using shock tunnels for aerothermodynamic investigations is the reproduction of real flight conditions of vehicles at a very low cost. This chapter is dedicated to measurement methods

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https://doi.org/10.1007/978-3-031-31561-9e fluid molecules occur. Due to the extremely high power requirement and the severe flow environment, the required test conditions can only be achieved in ground based impulse facilities. The most successful types of facility which are able to generate high enthalpy and high pressure hypersonic flow

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https://doi.org/10.1007/978-981-16-0147-7ronment characterized by strong shocks and high temperatures, and the flow in the hypersonic regime behaves quite differently from that at supersonic Mach numbers (Bertin in Hypersonic Aerothermodynamics. Washington DC, .; Park in Nonequilibrium Hypersonic Aerothermodynamics, Wiley, New York, .; And

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Alfonso Zamora Saiz,Ronald A. Zú?iga-Rojasdedicated centre for the research, among other domains of fluid dynamics, on the shock dominated phenomena. More often than not, the focus of the research is on the flow phenomena at high enthalpies, which are addressed using the impulse facilities—shock tubes and tunnels. Ever since its inception a

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