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 Soc Automotive Engrs -- Paper n 603 for meeting Oct 11-15 1955 8 p)
Stability and control of piloted aircraft at high altitudes
Soc Automotive Engrs -- J
Society of Automotive Engineers -- Journal ; 603 , n 9
1956
3 pages
Aufsatz (Zeitschrift)
Englisch
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Stability and control of piloted aircraft at high altitudes
Engineering Index Backfile | 1955
|STABILITY AND CONTROL OF PILOTED AIRCRAFT AT HIGH ALTITUDES
SAE Technical Papers | 1955
|AIAA | 2004
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