Aeronautics & Astronautics - Fluid & Thermal Sciences > Fluids: Page 6

No. 25611 Tangent upper and lower surfaces at trailing edge No. 25612 Tangent upper and lower velocities at the trailing edge No. 25613 Equal upper and lower velocities at equal distances at trailing edge No. 25614 Movement of a volume element in time No. 25615 Closed curve around an airfoil in a counterclockwise direction No. 25616 Airfoil with a trailing starting vortex in a second closed curve No. 25617 Nonlifting discrete sources No. 25619 Continuous source distribution No. 25620 Lifting airfoil with continuous vortex and source distribution No. 25621 Method of source panel No. 25622 Method of vortex panel No. 25623 Method of source panel No. 25624 Method of vortex panel No. 25625 Circle No. 25626 Airfoil No. 25627 Methods of finite difference/element No. 25628 Path from a to b No. 25629 Airfoil No. 25630 Jth panel No. 25631 Panel No. 25632 Panel No. 25633 Panel source per unit length No. 25634 Panels: ith and jth No. 25635 Flow over bump No. 25636 Four panel closed body No. 25651 Sphere of radius R No. 25665 Pinned at base, spring and damper attached beams,one with mass at end. No. 25886 Simple gyroscope No. 25887 End-pivoting bar of mass M is attached to rotating T-bar No. 25888 Gyropendulum No. 25889 Wobble plate No. 25891 Ellipse: axis a and b No. 25920 Asymptotic suction layer No. 25921 Two concentric cylinders No. 25922 Elliptic Cross section: Poiseuille flow No. 25923 Cylinder and ellipse: geometry of No. 25924 Pressure coefficient for a cylinder No. 25928 Pressure coefficient distribution: NACA 5412, 5 deg angle of attack No. 25929 Pressure coefficient distribution No. 25930 Airfoil geometry comparison No. 25931 Pressure coefficient distribution comparison No. 25932 Pressure coefficient distribution comparison No. 25933 Pressure coefficient distribution comparison No. 25934 Pressure coefficient distribution comparison
 

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