Increasing altitude causes deterioration of important flight characteristics; aerodynamic damping suffers as ratio of true to indicated air speed increases; adequate static stability becomes more difficult under adverse influence of high supersonic speed and high angle of attack; all of these problems are amenable to solution; but they will not be forthcoming unless designers are prepared to accept new configurations. (see also abstract in Soc Automotive Engrs -- J v 64 n 9 Aug 1956 p 25-7)
Stability and control of piloted aircraft at high altitudes
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1955 Supersonic speeds
1955
8 pages
Aufsatz (Konferenz)
Englisch
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Stability and control of piloted aircraft at high altitudes
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