首页> 外文会议>Instrumentation in Aerospace Simulation Facilities, 1997. ICIASF '97 Record., International Congress on >Background and prediction of correct full-scale reproduction in wind tunnels as concerns gas dynamic parameters of hypervelocity atmospheric flights and scramjet combustion chamber conditions
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Background and prediction of correct full-scale reproduction in wind tunnels as concerns gas dynamic parameters of hypervelocity atmospheric flights and scramjet combustion chamber conditions

机译:关于超高速大气飞行的气体动力学参数和超燃冲压燃烧室条件的风洞中正确全尺度繁殖的背景和预测

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The report analyzes possible schemes of aerodynamic rigs intended for reproducing gas dynamic parameters (velocity, density, pressure, and temperature) and chemical air composition as applied to the TAV trajectory with the indication of required stagnation parameters (P/sub 0/, T/sub 0/). Based on the calculation of physico-chemical processes taking place in nozzles of classical facilities it is inferred that the chemical air composition differs noticeably from the natural air composition even in solving the problem of producing and retaining the gas in the plenum chamber at ultrahigh temperatures and pressures (T/sub 0//spl ges/7000 K, P/sub 0//spl ges/4/spl middot/10/sup 8/ Pa). The analysis carried out reveals a distinct advantage of MHD-gas acceleration facilities in solving the stated problem. A set of equations of magnetogasdynamics and multitemperature physico-chemical kinetics which underlie the computation program is presented. The channels of energy transport from the electromagnetic field to the gas at different gas densities are considered. The program was compiled using the experimental data obtained in the TsAGI MHD-gas acceleration hypersonic wind tunnel. The report presents the calculated data on gas acceleration regimes in a wide spectrum of initial conditions and electrodynamic parameters. The consideration of nonequilibrium physico-chemical processes in the MHD-channel and in the secondary nozzle makes it possible to state that the nonequilibrium effects facilitate considerably the reproduction of a natural chemical air composition and a static temperature in the facility test section. The influence of alkali seeds on the induction time and hydrogen burning process in the scramjet combustion chamber is evaluated. Possible technical approaches to the realization of calculated versions of MHD-accelerators are analyzed.
机译:该报告分析了用于重现气体动力学参数(速度,密度,压力和温度)和应用于TAV轨迹的化学空气成分的空气动力学装置的可能方案,并指出了所需的停滞参数(P / sub 0 /,T /子0 /)。根据经典设施喷嘴中发生的物理化学过程的计算,可以推断出,即使解决了在超高温下在增压室中产生和保留气体的问题,化学空气成分也与天然空气成分明显不同。压力(T / sub 0 // spl ges / 7000 K,P / sub 0 // spl ges / 4 / spl middot / 10 / sup 8 / Pa)。进行的分析揭示了MHD气体加速设施在解决上述问题方面的独特优势。提出了计算程序基础的一组磁气动力学和多温度物理化学动力学方程。考虑了在不同气体密度下从电磁场到气体的能量传输通道。该程序是使用在TsAGI MHD气体加速高超音速风洞中获得的实验数据编译的。该报告介绍了各种初始条件和电动参数中有关气体加速状态的计算数据。考虑到MHD通道和辅助喷嘴中的非平衡物理化学过程,可以说明该非平衡效应大大促进了自然化学空气成分的再生和设施测试部分的静态温度。评估了碱金属种子对超燃喷射燃烧室中诱导时间和氢燃烧过程的影响。分析了实现MHD加速器计算版本的可能技术方法。

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