Erratum to: Aeroelastic stability analysis of flexible overexpanded rocket nozzle
نویسندگان
چکیده
منابع مشابه
Aeroelastic Modeling of a Nozzle Startup Transient
Lateral nozzle forces are known to cause severe structural damage to any new rocket engine in development during test. While three-dimensional, transient, turbulent, chemically reacting computational fluid dynamics methodology has been demonstrated to capture major side load physics with rigid nozzles, hot-fire tests often show nozzle structure deformation during major side load events, leading...
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ژورنال
عنوان ژورنال: Shock Waves
سال: 2016
ISSN: 0938-1287,1432-2153
DOI: 10.1007/s00193-016-0687-3