Aeronautics & Astronautics - Fluid Sciences > Aerodynamics: Page 13

No. 26073 Wingtip vortices No. 26074 Effect of downwash No. 26075 Biot-Savart law, vortex filament No. 26076 Infinite straight vortex filament induced velocity No. 26077 Induced velocity due to semi-infinite straight vortex filament No. 26078 Lift distribution across span of wing No. 26079 Bound vortex replacing a finite wing No. 26080 Single horseshoe vortex's downwash distribution No. 26081 Finite number of superposed horseshoe vortices along lifting line No. 26082 Infinite number of superposed horseshoe vortices along lifting line No. 26083 High-aspect-ratio wing No. 26084 Low Aspect-Ration wing No. 26085 Elliptic wing with elliptic lift and constant downwash No. 26086 Elliptic wing planform No. 26087 Rectangular wing No. 26088 Tapered wing planform No. 26092 Induced drag factor vs taper ratio for different aspect ratios No. 26093 Different aspect ratio data for Prandtl's classic rectangular wing No. 26094 Prandtl scaled data for an aspect ratio of 5 No. 26095 Lift coefficient vs effective angle of attack for infinite wing No. 26096 Lift coefficient vs angle of attack for finite elliptic wing No. 26097 Different aspect ratio data for Prandtl's classic rectangular wing No. 26098 Prandtl scaled data for an aspect ratio of 5 No. 26099 Spanwise stations for numerical solution No. 26100 Rectangular wing lift distribution No. 26101 Lift coefficient vs angle of attack experimental and numerical No. 26102 Straight low aspect ratio wing No. 26103 Lifting surface schematic No. 26104 Infinitesimal lifting surface segment induced velocity No. 26105 Single horseshoe vortex schematic No. 26106 Finite wing vortex lattice system No. 26107 Straight wings lift slope vs aspect ratio for low speed flow No. 26108 Swept wing geometry No. 26109 Space shuttle No. 26110 Planform of a simple delta-wing No. 26111 Planform of a cropped delta-wing No. 26112 Planform of notched delta-wing No. 26113 Planform of double delta-wing No. 26114 Subsonic flow field over top of delta wing at angle of attack No. 26115 Distribution of pressure coefficient along span of delta wing No. 26116 Lift coefficient variation with angle of attack for flat delta wing No. 26117 Lift-to-drag ratio for delta wing with aspect ratio of 2.31 No. 26118 Delta-wing top spanwise pressure coefficient distribution No. 26119 Finite wing's wing-tip vortex No. 26120 Point source in three dimensions No. 26121 Three-dimensional doublet No. 26122 zr plane streamlines for three-dimensional doublet No. 26123 Three-dimensional doublet and a uniform flow superposition No. 26124 Sphere's schematic of an incompressible flow No. 26125 3-D relieve effect of sphere & cylinder surface pressure distribution
 

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