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Showing 1 to 4 of 4 for “"symmetrical airfoils"”.

  1. Turbulence Interaction in a Highly Sataggered Cascade-Propulsor Configuration

    … cascade propulsor configuration formed by non-symmetrical airfoils. This present study was possible thank to the support from the Office of Naval Research, in particular Candace Wark and Pat Purtell, under grant number NAG 00014-99-1-0230.

    vt Repository record for Turbulence Interaction in a Highly Sataggered Cascade-Propulsor Configuration (opens in a new tab)

  2. Experimental wind tunnel study of airfoils with large flap deflections at low Reynolds numbers

    … were taken at low Reynolds numbers for four airfoils with trailing edge plain flaps in an attempt to understand the effects of Reynolds number, percent thickness (t/c), percent chord of flap (flap-chord ratio), and flap deflection on airfoil performance. The four airfoils used in this …

    uiuc Repository record for Experimental wind tunnel study of airfoils with large flap deflections at low Reynolds numbers (opens in a new tab)

  3. The turbulence structure of trailing vortex wakes

    … measurements. Vortices were generated using two symmetrical airfoils. Measurements were made in cross-sectional grids and profiles over a range of Reynolds numbers and downstream distances. Contours of axial normal stress were high-pass filtered to remove the contributions of wandering to the …

    vt Repository record for The turbulence structure of trailing vortex wakes (opens in a new tab)

  4. Experimental Investigation of Transonic Shock Oscillations on NACA 0018 at Incidence

    A NACA 0018 airfoil model with a 3-inch chord was mounted into the trisonic wind tunnel at the National Center for Physical Acoustics at the University of Mississippi. Tunnel runs were conducted with the angle of incidence increasing from 0 degrees to 6 degrees at 1 degree increments, while the …

    mississippi Repository record for Experimental Investigation of Transonic Shock Oscillations on NACA 0018 at Incidence (opens in a new tab)