Stability, control and handling problems resulting from drastic changes in aircraft configuration and advent of flight at high altitude; longitudinal and lateral characteristics of supersonic aircraft; design of flying control system and methods for solving various stability problems. From Quarterly Bul of Nat Aeronautical Establishment, Ottawa, Canada. (See also - n 342 Aug 1957 p 241-7; Can Aeronautical J v 3 n 5, 6 May 1957 p 146-51, June p 178-84)
Stability and control problems associated with supersonic aircraft
Aircraft Eng
Aircraft Engineering ; 29 , n 343
1957
7 pages
Article (Journal)
English
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