motion
Glenn
Research
Center
Newton’s Second Law with mass constant: F = m a F = Force =( Lift - Weight) or (Thrust - Drag) a = F / m
lf Force remains constant, acceleration is constant:
Aircraft Motion - Constant Force
Newton’s Second Law
V = a t + V0
X = ąjj + V0t + X 0
2
Wyszukiwarka
Podobne podstrony:
motion Glenn Research Center Newton’s Second Law with mass constant: F = m a F = F
isentrop Isentropic Flow Eguations Glenn Research Center Mach = M speed of sound = a gas consta
doppler Doppler Effecł Glenn Research Center Wavelength (I) X Freguency (f) = Speedof Sound (a) Leav
mflchk Compressible Mass Flow Ratę Glenn Research Center R = Gas Constant y =Specitic Fleat
presar Aerodynamic Forces Glenn Research Center Pressure forces act normal (perpendicular) to surfac
range Rangę - Constant Vetocity Glenn Research Center amount = ratę x time Ground Speed = V Distance
rud Yertical Słabilizer - Rudder Glenn Research Center Słabilizer Rudder
oblique Obligue Shock Eguations Glenn Research Center Mach =M Stagnation (Total) Conditions = t
density Density Effects on Aerodynamic Forces Glenn Research CenterF = Force L = Lift D = Drag
doppler Doppler Effecł Glenn Research Center Wavelength (I) X Freguency (f) = Speedof Sound (a) Leav
fwrat Thrust to Weight Ratio Research Center i 1 Lift - L Weight - W Thrust - F Drag- D F _ Th
Authentication Center (AuC): Physically exists with an HLR, as depicted in figurę 4. This component
Kavicsfestés I 56 Paint the center Switch to your large brush to fili in the center of the shape w
więcej podobnych podstron