Set up a kinetic analysis model to study ground-maneuver-stability of multiple-bogie undercarriage. The calculations and simulations demonstrate that the allowable nose wheel steering angle and aircraft's ground-maneuver stability could be improved by decreasing height of C.G of aircraft, increasing aircraft's weight, decreasing aircraft's velocity and decreasing engine thrust on condition that aircraft's configuration is identical and aircraft's safety and performance do not reduce.
A study of ground maneuver stability of multiple-bogie undercarriage
2016-10-01
304559 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Machining Undercarriage Bogie Beams
Emerald Group Publishing | 1983
Landing loads on Bogie undercarriage
Engineering Index Backfile | 1952
|Semi-articulated multi-wheel Bogie undercarriage
Engineering Index Backfile | 1951
|Semi-Articulated Bogie Undercarriage Landing Performance
Emerald Group Publishing | 1959
|Landing Loads on the Bogie Undercarriage
Emerald Group Publishing | 1952
|