The article is devoted to the analysis of the trajectory parameters obtained during the flight experiment at the start of meteo-rocket MMP-06, to determine major parameters of motion of a round parachute at subsonic speeds in the range of altitudes from 0 to 60 km. The Reynolds number is changed in the range from 104 to1,5·106.The main parameters of the trajectory were obtained according to the experimental data. Only laboratory research on a model parachute systems in such a wide range of Reynolds numbers are found in the literature on parachute subjects. This article obtained results of flight experiment.
PROCESSING AND ANALYSIS OF DATA OF natural experiment FOR DETERMINING THE tragectory CHARACTERISTICS OF A ROUND PARACHUTE AT HIGH ALTITUDES
2016
Article (Journal)
Electronic Resource
Unknown
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