The statistical approach to the gust-loads problem, which consists in considering flight th1ough turbulent air to be a stationary random process, is extended by including the effect of lateral variations of the instantaneous gust intensity on the aerodynamic forces and on the resultant motions and stresses of rigid and flexible airplanes. By means of some calculations of normal and rolling accelerations, as well as of the root bending moment, it is shown that these effects may be significant for large airplanes.
The Dynamic Response of a Large Airplane to Continuous Random Atmospheric Disturbances
23rd Annual Institute of the Aeronautical Sciences (IAS) Meeting ; 1955 ; New York, NY, US
Journal of Aeronautical Sciences ; 23 , 10
1956-10-01
Miscellaneous
No indication
English
Dynamic response of large airplane to continuous random atmospheric disturbances
Engineering Index Backfile | 1956
|The response of an airplane to random atmospheric disturbances
TIBKAT | 1958
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