The aircraft for which the stalling speed Vs in level flight is 52.5 m/s has a maximum
Fantastic news! We've Found the answer you've been seeking!
Question:
The aircraft for which the stalling speed Vs in level flight is 52.5 m/s has a maximum allowable maneuver load factor n1 of 3.61. In assessing gyroscopic effects on the engine mounting, the following two cases are to be considered:
(a) Pull-out at a maximum permissible rate from a dive in symmetric flight, the angle of the flight path to the horizontal being limited to 60o for this aircraft.
(b) Steady, correctly banked turn at the maximum permissible rate in horizontal flight. Find the corresponding maximum angular velocities in yaw and pitch.
Related Book For
Vector Mechanics for Engineers Statics and Dynamics
ISBN: 978-0073212227
8th Edition
Authors: Ferdinand Beer, E. Russell Johnston, Jr., Elliot Eisenberg, William Clausen, David Mazurek, Phillip Cornwell
Posted Date: