The development of a vector wind gust model through statistical analysis is described. Wind perturbation statistics which include location, altitude, season, and wavelength range are used in the synthesis of detailed wing profiles. These profiles provide the basis for the establishment of improved discrete gust design criteria guidelines for ascending launch vehicles.
Vector wind gust model
1984-04-13
Report
Keine Angabe
Englisch
UAS-based Wind Estimation Using Sinusoidal Gust Model
AIAA | 2019
|Engineering Index Backfile | 1966
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