Papers Published

  1. Reynolds, Robert R. and Dowell, Earl H. and Tang, Deman and Virgin, Lawrence N., Nonlinear behavior of low aspect ratio panels in subsonic flow: a preliminary study, American Society of Mechanical Engineers, Aerospace Division (Publication) AD, vol. 33 (1993), pp. 9 - 12 .
    (last updated on 2007/04/10)

    We describe an experimental investigation into the nonlinear behavior of thin elastic panels in subsonic flow. Specially, an apparatus is detailed that supports a low aspect ratio panel by clamping it along the spanwise edges while leaving its leading and trailing edges free. Preliminary results are given for a 0.016 inch thick panel with an aspect ratio of 2.72. A pronounced, leading-edge divergence phenomenon was observed at nonzero angles of attack.

    Aerospace engineering;Flutter (aerodynamics);Subsonic flow;