首页> 外文会议>Ninth international conference on sound and vibration (ICSV9) >SELF-SUSTAINED JET OSCILLATION PHENOMENA RELATED TO AXISYMMETRIC ROCKET JETS INTERACTION DURING TAKE-OFF
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SELF-SUSTAINED JET OSCILLATION PHENOMENA RELATED TO AXISYMMETRIC ROCKET JETS INTERACTION DURING TAKE-OFF

机译:与起飞时轴对称火箭弹相互作用有关的自持式射流振荡现象

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Powerful self –sustained oscillations of axisymmetric set of rocket jets are predicted duringrntake-off, slow lift and initial stage of flight due to jets interaction with symmetric take-offrntable construction elements, such as rocket supporting ring and mutual jet interaction duringrninitial stage of flight. Discrete jets system is modeled by continuos circular jet issuing out ofrncircular orifice in an impedance plate. Circular jet could either collapse in unconfined space orrninteract with symmetric take-off table elements (say, rocket-supporting ring). Both kinds of jetrninteraction lead to generation of volume- flow sources formed in the region of jet collision orrnobstacle interaction. These sources production rates are related directly to jet deflectionsrninside or outside inner jet-bounded axisymmetric volume. Values of jet roots deflection inrntheir turn are governed by system of axial standing acoustic waves formed in sad volume. Byrnmeans of Nyquist stability criteria (both phase and amplitude) conditions of self-sustainedrnloop process in axisymmetric volume are derived and their dependence on system parametersrnare determined. Subsonic and supersonic jet flow cases are analyzed. Slowly changing central oscillation frequency with system lift (narrow band) oscillation phenomenon is thus predicted.rnPredictions are compared to available experimental data.
机译:在喷气飞机起飞,缓慢升力和飞行初始阶段,由于喷气飞机与对称可起飞结构元件的相互作用,例如火箭支撑环和初始飞行阶段的相互喷气机相互作用,预计在起飞,缓慢升起和飞行初始阶段,轴对称喷气飞机会产生强大的自持振荡。离散射流系统是通过从阻抗板上的圆孔喷出的连续圆形射流建模的。圆形射流可能在无限制的空间中坍塌,或者与对称的起飞台元件(例如,火箭支撑环)相互作用。两种射流相互作用都导致在射流碰撞或障碍物相互作用区域内形成体积流源。这些源的生产率直接与内部射流边界内或外部射流界定的轴对称体积内的射流挠度直接相关。射流根偏斜度的值由在悲伤体积中形成的轴向驻波系统控制。推导了轴对称体积中自持环过程的奈奎斯特稳定性标准(相位和幅值)的By均值,并确定了它们对系统参数的依赖性。分析了亚音速和超音速射流情况。因此,可以预测随着系统提升(窄带)振荡现象中心振荡频率的缓慢变化。rn将预测值与可用的实验数据进行比较。

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