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The aerodynamic analysis of the gyroplane rotating-wing system

NASA Technical Reports Server (NTRS) · 1934 · 1 picture

A 1934 NASA technical report on gyroplane rotating-wing aerodynamics, issued as a government research document for aeronautical engineers. Its single picture is a technical graph of propeller thrust coefficients against resultant and translational velocity, with a rounded curve splitting into windmill-decelerating and vortex-ring branches on a fine grid with labelled axes. A designer might take from it the clean, minimal chart style: thin black curves, dotted leader arrows, and plain serif labels on white.

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work) · More from this library