Aeronautics & Astronautics - Fluid Sciences > Aerodynamics: Page 8

No. 30121 Variations in flow field around blunt-nose body No. 30122 High temperature shock wave in blunt body at hypersonic flow No. 30123 Drag coefficient vs. Knudsen number No. 30124 Numerical solution methods and their equations vs. Knudsen number No. 30125 Newton's law for hypersonic flow: incident angle No. 30126 Newton's law for hypersonic flow: incident flow No. 30127 Thin shock layer in hypersonic flow No. 30128 Balance equations prior and after shock front No. 30129 Hypersonic Newtonian theory No. 30130 Fraction of lift over drag versus angle of attack No. 30131 Evaluating drag coefficient of circular body in 2-D flow No. 30132 Shock wave due to flow compression induced by inclined path No. 30133 Shock wave and flow path inclination angles No. 30134 Pressure distribution: comparison of wedge and cone No. 30135 Flat plate with incident flow at zero pressure No. 30136 Mach number independence: flows over sphere and cylinder No. 30137 Hypersonic expansion wave No. 30138 Streamline along with two characteristic lines No. 30139 Intersecting two characteristic lines No. 30140 Streamline and intersecting characteristic lines No. 30141 Reference plane method in 3D flow analysis over conical bodies No. 30142 Shock wave analysis over conical body: downstream solution No. 30143 Grid points on lines perpendicular to body surface for flow analysis No. 30144 Domains of influence and dependence in flow analysis No. 30145 Method of characteristics: domains of dependence-influence No. 30146 Flow through converging and diverging ducts No. 30159 Normal isentropic exit in nozzle flow No. 30160 Flow expansion at nozzle exit No. 30161 Flow over super-critical airfoil No. 30162 Vortex source and collocation point for boundary conditions No. 30225 Elliptic chordwise vorticity distribution representing 2D airfoil No. 30226 Lifting surface theory: concentrated vortex at quarter chord airfoil No. 30227 Tandem airfoils at angle of attack No. 30228 Constant strength doublet distribution No. 30229 Octagon representation for cylindrical body No. 30230 Cylindrical body for approximate analysis No. 30231 Construction of panels for cylindrical body representation No. 30232 Cylindrical body close to wall for approximate analysis No. 30233 Hinged thin symmetric airfoil at small angle of attack in free stream No. 30263 NACA 4415 airfoil mounted on rod to determine moment at pivot point No. 30264 NACA 4415 lift coefficient as function of angle of attack No. 30265 NACA 4415 drag versus lift coefficients No. 30266 Shape factor with curve fit of laminar boundary layer function No. 30267 Shear stress with curve fit of laminar boundary layer function No. 30278 Elliptical loading on slender wing with rectangular planform No. 30279 Angle of attacks along rectangular wing for elliptical load No. 30280 Circular cone: aerodynamic moment about cone vertex No. 30281 Biplane wing No. 30282 Monoplane wing No. 30283 Counterclockwise roll generated by ailerons
 

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