Static longitudinal stability and longitudinal control of autogiro rotors (1938)
NASA Technical Reports Server (NTRS) · leaf 20
V.A.C.A. Teotanlcal Uemorandim Ho. 879 71g8. 12,13,14,15,16 =..2.40 Vigore 12.- Blade euod control Burface momentB for blade control. !Ehe double airrows Indicate tlie related lines and the point of the corresponding moment 100c; .balance. a , degrees … Tlgure 15.- Blade'anfcontrol surface moments with "gravity control". 6 .10 5 .05 lOOCm 4 0 3 -.05 K.v=l 20 15 5 10 2 a ,degrees 71gure 16.- Total moments with "gravity control"* -1 -2 -3 figure 14.- Belatlon between speed and control deflection for "blade control" and "gravity control". The control…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
