The distance an airplane floats with respect to the ground during deceleration at constant altitude is analyzed taking into account the effects of a constant wind. By use of suitable nondimensionalizing parameters, data applicable to all airplanes are presented by means of a single family of curves.
Ground Distance Covered During Airborne Horizontal Deceleration of an Airplane
1978
13 pages
Report
No indication
English
Limiting payload deceleration during ground impact
AIAA | 1983
|Limiting payload deceleration during ground impact
AIAA | 1981
|