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Доник, В.Д.; НАУ, кафедра безпеки життєдіяльності (2006)
Publisher: National Aviation University
Languages: Ukrainian
Types: Unknown
Subjects:
 Theoretical and experimental researches of the aerodynamic processes during gas outflow from the vessel via gap have been developed. For the first time were obtained an mathematical models as well as were actually researched the unsteady gas outflow processes at the positive and negative gas impact exerted on the shield. Were considered gas flow modes in the gap between vessel and shield; the calculation results were compared with experimental one.  Приведены результаты теоретических и экспериментальных исследований аэродинамических процессов течения газа из сосуда через зазор. Рассмотрены режимы течения газа в зазоре между сосудом и экраном.  Наведено результати теоретичних й експериментальних досліджень аеродинамічних процесів течії газу із посудини через зазор. Розглянуто режими течії газу в зазорі між посудиною й екраном.
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