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50a m 1220p m
Droplet Vaporization in a Stationary Cloud at Sub and Super
Moments of the Aircraft
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acoustic aerodynamic AIAA aircraft airfoil amplitude analysis angle of attack anorthite applied axial base bleed beam boundary conditions boundary layer buckling cement characteristics coefficient combustion composite compressive computed configuration coordinate cryogenic deflection delamination developed diffusion flame distribution drag drag coefficient droplet dynamic effect end milling Engineering equations excitation experimental fiber waviness Figure finite element flow field Fluid forcing fuel function grid heat increases integral interaction iteration laminate lift lift coefficient load lunar concrete LUNAR-A Mach number material matrix measurements mechanism method mode mode shape natural frequency noise obtained optimal control orbit parameters particle plate pressure problem ratio region Reynolds number sandwich panel scheme shear layer shock shown in Fig simulation solution spoiler spray stability structure surface technique temperature thermal tion transonic transverse turbulence unsteady variables vector velocity vibration vortex vorticity wall wave wind tunnel