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pro vyhledávání: '"Donald T. Reynolds"'
Autor:
William M. Mullins, Donald T. Reynolds
Publikováno v:
Journal of Spacecraft and Rockets. 8:1068-1073
An analytical method has been developed for determining the unique shape and internal load distribution that satisfies equilibrium and boundary conditions for a parachute under the influence of known riser and aerodynamic forces. The parachute is tre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3cbc58492bc5dc7695d318e20ecf9b32
https://doi.org/10.2514/3.59768
https://doi.org/10.2514/3.59768
