To improve the operation efficiency of conventional Ludwieg tube tunnel, a fast-acting valve
is usually deployed between the storage tube and Laval nozzle in order to separate the high …

State-to-state simulations of nonequilibrium flow in nozzles are made for a range of reservoir
conditions and geometries. The geometry of the converging section and throat has little …

高超声速风洞是研究高超声速空气动力学关键问题的重要手段, 但是常规高超声速风洞建设和
运行成本偏高, 不利于深入开展高超声速飞行器部分空气动力学基础问题研究 …

Afterbody flow phenomena represent a significant source of uncertainties in the design of a
launcher. Therefore, there is a demand for measuring such flows in wind tunnels. For …

Plasma assisted CO 2 dissociation has recently been the topic of many studies. The
production of chemical fuels from environmentally unfriendly CO 2 through supersonic …

Ludwieg 管风洞能低成本, 高效率地产生低湍流度的高超声速气流, 被广泛用于高超声速(马赫数
6 及以上) 基础空气动力学实验研究. 尽管Ludwieg 管式高超声速风洞逐渐普及 …

高超声速边界层层/湍流转捩是高超声速飞行器气动力和气动热设计中的难点和热点问题.
为了降低开展高超声速边界层不稳定性与转捩实验研究的门槛, 研究基于Ludwieg …

RANS simulations of a tandem nozzle supersonic wind tunnel with perforated plates
installed in the settling chamber are presented in this paper. For the sake of obtaining more …

A simulative method for quantifying the discharge process of cold gas airbag inflators is
presented. The pressure, mass flow and the influences of the flow field are relevant to a …

The flow characteristics of the tandem nozzle supersonic wind tunnel at the Institute of Fluid
Mechanics, Technische Universität Braunschweig, a are investigated. Conventional …