The advantages of the control configured vehicle concept compared to conventional aircraft design, are pointed out for several examples. The improvements are found especially in the specific performance surplus at high lift coefficients, and in an increase of the obtainable maximal lift coefficients. The dynamic flight characteristics of these aircraft can be made similar to or better than aerodynamically stable aircraft by a suitable artificial stabilization. (Author)
Efficiency Increase by Control System Supported Aircraft Design . Leistungserhoehung durch Reglergestuetzten Flugzeugentwurf
1972
28 pages
Report
Keine Angabe
Englisch
Gewichtsabschaetzungsmethodik fuer den Flugzeugentwurf
Tema Archiv | 1974
|Gewichtsabschaetzungsmethodik fuer den Flugzeugentwurf
Kraftfahrwesen | 1974
|Ueber Methoden der Systemtechnik beim Flugzeugentwurf
Engineering Index Backfile | 1968
|Die Berechnung von Strukturgewichten fuer den Flugzeugentwurf
Engineering Index Backfile | 1967
|