Thought I'd share this find -- discovered it just now:
http://ntrs.nasa.gov/
Document-ID: 19770018207
Title: US Army helicopter design datcom. Volume 1 Airfoils
Author: Leo Dadone
Abstract:
        This report contains airfoil data of interest for rotor
        applications. The data is presented in the form of lift, drag, and
        pitching moment coefficients and, in most cases, it covers the
        complete Mach number range from low subsonic to supercritical flow
        conditions. An introductory section presents airfoil data trends
        and information pertaining to the source and usefulness of such
        data.

The pdf is >19MB

No traces of a volume 2 at NTRS. Maybe there never was one.

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