Dynamic instability of rockets fairings
Heading:
| 1Avramov, KV, 1Chernobryvko, MV, 2Batutina, TYa., 3Degtyarenko, PG, 2Tonkonozhenko, AM 1A. N. Podgorny Institute for Mechanical Engineering Problems of the National Academy of Sciences of Ukraine, Kharkiv, Ukraine 2Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine 3Yangel Yuzhnoye State Design Office, Dnipro, Ukraine |
| Kosm. nauka tehnol. 2015, 21 ;(1):10–14 |
| https://doi.org/10.15407/knit2015.01.010 |
| Publication Language: Russian |
Abstract: : Aeroelastic vibrations of rockets fairing, which are parabolic or conic shells, are considered. These shells are faded-in by stringers and rings. The dynamic instability of such structures in supersonic gas stream is analyzed. |
| Keywords: ring-stiffened conical shells, shell space mode, supersonic gas stream, vibrations of rocket deflector |
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