Wind Tunnel Measurements At Subsonic Speeds Of The Static And Dynamic Rotary Stability Derivatives Of A Triangular Wing Airplane Model Having A Triangular Vertical Tail
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Wind-tunnel measurements at subsonic speeds of the static and dynamic-rotary stability derivatives of a triangular-wing airplane model having a triangular vertical tail
Wind-tunnel measurements at subsonic speeds of the static and dynamic-rotary stability derivatives of a triangular-wing airplane model having a triangular vertical tail.
NASA Memorandum
Author: United States. National Aeronautics and Space Administration
language: en
Publisher:
Release Date: 1958