research

WIND-TUNNEL MEASUREMENTS OF AERODYNAMIC DAMPING DERIVATIVES OF A LAUNCH VEHICLE VIBRATING IN FREE-FREE BENDING MODES AT MACH NUMBERS FROM 0.70 TO 2.87 AND COMPARISONS WITH THEORY

Authors
Publication date
Publisher

Abstract

Wind tunnel tests of aerodynamic damping of a launch vehicl

    Similar works

    Full text

    thumbnail-image

    Available Versions

    NASA Technical Reports Server

    redirect
    oaioai:casi.ntrs.nasa.gov:1962000...
    Last time updated on 15/04/2017