Low-speed Investigation of the Effects of Single Slotted and Double Slotted Flaps on a 47.7 Degree Sweptback-wing : Fuselage Combination at a Reynolds Number of 6.0 x 10(exp 6)

Authors
Publication date
Publisher

Abstract

Abstract is not available.

    Similar works

    Full text

    thumbnail-image

    Available Versions

    NASA Technical Reports Server

    redirect
    oaioai:casi.ntrs.nasa.gov:1993008...
    Last time updated on 03/08/2016