Aeronautics & Astronautics - Fluid Sciences > Aerodynamics: Page 9

No. 30284 Horseshoe vortices generated by wings No. 30285 Vortex generated by line segment No. 30287 Pressure distribution of NACA 0008 airfoil at zero angle of attack No. 30288 Pressure distribution of NACA 0008 airfoil at nonzero angle of attack No. 30289 Pressure distribution of NACA 2408 airfoil at zero angle of attack No. 30290 Pressure distribution of NACA 2408 airfoil at nonzero angle of attack No. 30354 Evaluating free-stream mach number of flow over diamond airfoil No. 30355 Two dimensional scramjet inlet No. 30356 Shock wave and deflection angles of NACA 1135 airfoil No. 30357 Shock wave and deflection angles of NACA 1135 airfoil No. 30358 Downstream Mach number vs. deflection angle on NACA 1135 No. 30359 Downstream Mach number vs. deflection angle on NACA 1135 No. 30360 Finding ratio of max thickness and chord length for minimum drag No. 30361 Contour function of elliptical airfoil No. 30362 Elliptical airfoil at angle of attack No. 30363 Sinusoidal wall: potential function for subsonic and supersonic flows No. 30388 Surface pressure coefficient vs. cone semivertex angle No. 30389 Surface pressure coefficient vs. cone semivertex angle No. 30390 Sine wave propagated through long tube No. 20759 Streamline flow over an airfoil No. 20760 Stagnation points and streamline No. 20761 Constant properties at station 1 and 2 No. 20762 Stream tube in air flow over an airfoil No. 20763 Cube overview and sideview dimensionals No. 20764 Pitot-Static tube and manometer characteristics No. 20765 Airspeed reading system schematic No. 20766 Characteristics of a low-speed wind tunnel No. 20767 Flow over an airfoil No. 20768 Lift, drag and total aerodynamic force on an airfoil No. 20769 Chordwise distribution of streamtube velocity above and below airfoil No. 20770 Chordwise upper and lower surface pressure distribution No. 20771 Lift and normal force on airfoil No. 20772 Airfoil surface pressures No. 20773 Force component due to surface pressure normal to the chord No. 20774 Velocity profile of a boundary-layer No. 20775 Transition and separation of boundary layer No. 20776 Velocity profiles of laminar and turbulent boundary layers No. 20777 Smooth surface No. 20778 Dimpled surface No. 20779 Parameters of an airfoil shape No. 20780 Wind-tunnel test section showing top view of rectangular wing section No. 20781 Front view of rectangular wing section in wind-tunnel test section No. 20782 Side view of rectangular wing section in wind-tunnel test section No. 20783 Symmetrical airfoil No. 20784 Attack's angle on a symmetrical airfoil No. 20785 Attack's angle on a symmetrical airfoil No. 20786 Lift coefficient for symmetrical airfoil No. 20787 Drag coefficient for symmetrical airfoil No. 20788 Zero angle's attack on a cambered airfoil No. 20789 Lift coefficients for cambered and symmetrical airfoils
 

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