The Effect on Rudder Control of Slip Stream Body, and Ground Interference (1922)
NASA Technical Reports Server (NTRS) · leaf 10
~Yawing Moment, N =gnu cm. Yawing Moment,N = gnu cm. 6€>00 8CCC GC CO 6GCO 4CCC C DC c c c "2 C C C 40CO KCC 6CCC 6CCC 8 C C C 8G0C c c o o o C +10 2 0 Rudder angle. Rudder angle. Fig. 4 - No.l model two chord Fig. 3 - No. 1 model without lengths above ground. No slip- interference.No slip-stream-… … Rudder angle. Rudder Angle. Fig.5- No-2 model. Three point Fig.6- Comparison of rudder control landing. No slip-stream. 13.5* for different bodies and slip-strearr angle of attack. conditions. 32.5C angle of attack.
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