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Wind-Tunnel Investigation at Supersonic Speeds of a Canard-Controlled Missile with Fixed and Free-Rolling Tail Fins

Title:Wind-Tunnel Investigation at Supersonic Speeds of a Canard-Controlled Missile with Fixed and Free-Rolling Tail Fins
Author:
Note:NASA Technical Paper 1316; 1978
  
Link:
Stable link here:https://onlinebooks.library.upenn.edu/webbin/book/lookupid?key=olbp62504
  
Subject:Rolling (Aerodynamics)
Subject:Guided missiles -- Control systems
Subject:Spoilers (Airplanes)
Subject:Aerodynamics, Supersonic
Other copies:Look for editions of this book at your library, or elsewhere.

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