Aeronautics & Astronautics - Fluid Sciences > Gas Dynamics: Page 1

No. 28095 Aero-assisted orbital transfer vehicle at low lift/drag configuration No. 28103 Thin shock layer - shock detachment in hypersonic flow on blunt body No. 28104 Temperature profile in hypersonic flow over flat plate No. 28105 Viscous interaction effect in hypersonic flow over sharp cone No. 28106 Plasma ionization phenomena in hypersonic flow past blunt body No. 28107 Temperature behind shock as function of freestream Mach number No. 28108 Flow equations: validity regimes No. 28109 Hypersonic flow over flying body: physical effects No. 28110 Force diagram on vehicle during reentry No. 28111 Flight paths for atmospheric rentry on velocity-altitude phase map No. 28112 Velocity-altitude phase map with lines of constant Mach numbers No. 28113 Geometry of oblique shock wave No. 28114 Diagram of shock wave-deflection angles at various Mach numbers No. 28115 Expansion wave as flow past diverging path No. 28116 Newtonian impact theory: incident flow stream at angle of attack No. 28117 Inclined surface area with respect to freestream flow No. 28118 Ratio of lift and drag as function of angle of attack: flow over plate No. 28119 Stagnation pressure variation as function of freestream Mach numbers No. 28120 Surface pressure distribution of blunt body No. 28121 Fluid element experiencing centrifugal force No. 28122 Shock layer model for centrifugal force according to Newtonian theory No. 28123 Surface pressure distribution on circular body impacted by flow No. 28124 Surface pressure distribution on biconvex 10% thick airfoil No. 28125 Surface pressure distribution on biconvex 10% thick airfoil No. 28126 Pressure coefficient on sharp wedge and cone: exact vs. Newtonian No. 28127 Tangent-wedge method No. 28128 Tangent-cone method No. 28129 Surface pressure distribution as function of slenderness ratio No. 28130 Pressure distribution computation: characteristics vs. shock expansion No. 28131 Pressure distribution over a given body at supersonic flow No. 28132 Pressure distribution over a given body at hypersonic flow No. 28133 Plots of drag coefficient for sphere and cone-cylinder No. 28134 Pressure distribution over a given cylinder: hypersonic similarity No. 28135 Pressure distribution over a given cylinder: hypersonic similarity No. 28136 Cone at angle of attack No. 28137 Cross section of cone at angle of attack No. 28138 Pressure of cone surface at angle of attack No. 28139 Cone surface pressure: comparison of theoretical results No. 28140 Cone surface pressure: Rasmussen's formula at some parameters No. 28141 Slope of normal force coefficient for slender cones: comparison No. 28909 Cell size effect on pressure distribution: leading-edge supersonic No. 28910 Cell size effect on friction distribution: leading-edge supersonic No. 28911 Formation of vortices: streamlines stage 1 No. 28912 Formation of vortices: streamlines stage 2 No. 28913 Formation of vortices: streamlines stage 3 No. 28914 Formation of vortices: streamlines stage 4 No. 28915 Formation of vortices: streamlines stage 5 No. 28916 Formation of vortices: streamlines stage 6 No. 28917 Center vortex velocities for various Knudsen numbers
 

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