Investigation of the lift, center of pressure, and drag of a projectile at a Mach number of 8.6 and a Reynolds number of 17 million

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