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 5 May 1957 p 146-51; Aircraft Eng v 29 n 342, 343 Aug 1957 p 241-7, Sept p 275-81)
Stability and control problems associated with supersonic aircraft
Can Aeronautical J
Canadian Aeronautical Journal ; 3 , n 6
1957
7 pages
Article (Journal)
English
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