Applied Aerodynamics |
´Ù¸¥ »ç¶÷µéÀÇ ÀÇ°ß - ¼Æò ¾²±â
¼ÆòÀ» ãÀ» ¼ö ¾ø½À´Ï´Ù.
¸ñÂ÷
OUTLINES OP THE DEVELOPMENT OP | 7 |
AIRSCREWS | 9 |
downwash wing moment | 42 |
ÀúÀÛ±Ç | |
Ç¥½ÃµÇÁö ¾ÊÀº ¼½¼Ç 15°³
±âŸ ÃâÆÇº» - ¸ðµÎ º¸±â
ÀÚÁÖ ³ª¿À´Â ´Ü¾î ¹× ±¸¹®
aerodynamic aerofoil aeronautics aeroplane aircraft airscrew airship anemometer angle of incidence angular velocity aspect ratio autogyro axes axis B.HP body boundary layer calculation centre of gravity centre of pressure chord coarse pitch constant corresponding curve cylinder deduced density diagram diameter difference direction downwash drag coefficient drag lb effect engine equal equation experiment experimental flaps closed flaps open flow round fluid given horizontal horsepower illustrated inclination increase indicated kite wire leads level flight lift coefficient load longitudinal balance maximum measured motion normal observed obtained plane position potential flow produced quantities relation resistance resultant force revolutions Reynolds rotation rudder seen shock wave shown in Fig shows similar skin friction Speed m.p.h. spin stalling steady stream stream-lines surface Table tailplane tests theory thrust trailing edge trailing vortices tube turbulence variations viscosity vortices weight whilst wind tunnel wing zero