The effects of wind shear on aircraft flying through thunderstorm gust fronts were investigated. A computer program was developed to solve the two dimensional, nonlinear equations of aircraft motion, including wind shear. The procedure described and documented accounts for spatial and temporal variations of the aircraft within the flow regime. Analysis of flight paths and control inputs necessary to maintain specified trajectories for aircraft having characteristics of DC-8, B-747, augmentor wing STOL, and DHC-6 aircraft was recorded. From the analysis an attempt was made to find criteria for reduction of the hazards associated with landing through thunderstorm gust fronts.
Investigations of simulated aircraft flight through thunderstorm outflows
1978-09-01
Report
No indication
English
Flight through thunderstorm outflows
NTRS | 1978
|Flight through thunderstorm outflows
AIAA | 1979
|Flight through thunderstorm outflows
NTRS | 1979
|