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On matrix boundary value problems 424
Wall effects in cavity flowI 151
A method for obtaining the characteristic equation of a matrix
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airfoil amplitude applied approximation arbitrary arc of trajectory assumed asymptotic axis boundary conditions boundary value problem bounded branch calculation coefficients components computation consider constant convergence coordinates corresponding curve cylinder defined deformation denote derivatives determined diagonalizing operator differential equation discussed distribution elastic expression finite flow fluid follows formula function given Hence hodograph inequality infinite initial integral curves integral equation interior interval limit limiting Mach linear Mach number Mach wave Math mathematical matrix mesh method motion noise normal obtained oscillating parameter partial differential equations plane plastic potential problem region relation represents respectively saddle point satisfy shear stress shown in Fig singular points sinh solution strain stream function stress supersonic surface symmetric temperature theorem theory transformation vanishes variables vector velocity velocity potential viscous wave wing zero