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Controlling Supersonic Boundary Layer Stability by Means of Distributed Mass Transfer through a Porous Wall

机译:通过多孔壁的传质控制超声速边界层的稳定性

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The interaction between disturbances in a compressible boundary layer in the presence of distributed mass transfer (injection or suction) through a permeable porous wall is considered in the linear and nonlinear approximations (weakly nonlinear stability theory). The regimes of moderate and high supersonic velocities (Mach numbers M = 2 and 5.35) are studied. The boundary conditions for the disturbances on a permeable wall are derived with account for the gas compressibility in pores and the presence of a suction chamber. Maximum pore dimensions, at which the surface properties have no effect on the disturbance characteristics, which are stabilized upon suction and destabilized upon injection, are determined. When the surface properties are taken into account, intense growth of the first-mode vortex disturbances occurs, which can completely undo the stabilizing effect of the suction. Injection leads to the vortex and acoustic mode destabilization on the linear range and the enhancement of the nonlinear processes on the transitional range.
机译:在线性和非线性近似(弱非线性稳定性理论)中,考虑了存在于通过可渗透多孔壁的分布质量传递(注入或吸力)的情况下,可压缩边界层中扰动之间的相互作用。研究了中等和高超声速(马赫数M = 2和5.35)的状态。考虑到孔隙中的气体可压缩性和存在抽吸室,得出了可渗透壁上扰动的边界条件。确定最大孔尺寸,在该尺寸下表面特性对干扰特性没有影响,该最大孔径在吸力时稳定,在注入时不稳定。当考虑到表面特性时,发生第一模式涡旋扰动的强烈增长,这可能完全消除吸力的稳定作用。注入会导致线性范围内的涡旋和声模失稳,并导致过渡范围内的非线性过程增强。

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