uwochris
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- Joined
- Dec 21, 2001
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Kigair,
From the book "Flight Theory For Pilots" by Charles Dole, (page 210):
"Note that the load factors required to fly at constant altitude in turning flight were determined by assuming that the wing of the a/c provided all the lift. According to this analysis, the load factor at 90 degress will be infinity and thus impossible to attain...the secret is of course that lift is provided by parts of the a/c other than the wings. If the nose is held above the horizontal, the vertical component of thrust will act as lift. The fuselage is also operating at an effective AOA and will also develop lift. The vertical tail and rudder will also develop lift."
From the book "Flight Theory For Pilots" by Charles Dole, (page 210):
"Note that the load factors required to fly at constant altitude in turning flight were determined by assuming that the wing of the a/c provided all the lift. According to this analysis, the load factor at 90 degress will be infinity and thus impossible to attain...the secret is of course that lift is provided by parts of the a/c other than the wings. If the nose is held above the horizontal, the vertical component of thrust will act as lift. The fuselage is also operating at an effective AOA and will also develop lift. The vertical tail and rudder will also develop lift."