The variable-geometry features of the United States supersonic transport are described. Particular attention is given to the hardware development of those variable-geometry features unique to the supersonic transport. The design, development, and current status of a direct lift control sys tern, the supersonic internal-external compression inlet, and the full-scale wing pivot are described.
Variable Geometry in a Supersonic Transport Aircraft
Sae Technical Papers
Aeronautic and Space Engineering and Manufacturing Meeting ; 1967
1967-02-01
Conference paper
English
Variable geometry in supersonic transport aircraft
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