Low-speed static longitudinal stability characteristics of a canard model having a 60 degrees triangular wing and horizontal tail
Description:
Report presenting an investigation of the low-speed, power-off static longitudinal stability and control characteristics of a canard model with a triangular wing and horizontal tail in the free-flight tunnel. Results regarding the horizontal tail used to overcome change in stability and horizontal tail used for longitudinal control are provided.
Date:
November 9, 1949
Creator:
Bates, William R.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department