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Anonymous  Post time 6 day(s) ago |Read mode
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https://doi.org/10.1007/978-981-15-5862-7_3
Analysis of Stepped Beam Using Reduced Order Models


https://doi.org/10.1134/S1028335821050025
Analytical Estimates of the Motion and Elastic Vibrations of the Structures of Separated Fairing Flaps of Rocket-Space Systems


https://doi.org/10.1134/S1028335823050026
Dynamic Model of the Separation of Large-Sized Elastic Structures


https://doi.org/10.1007/978-3-032-11549-2_47
Dynamic Loads Induced on the Satellite Launch Vehicle During Movement from Integration Facility to Launch Pad


https://doi.org/10.1007/978-981-15-5862-7_25
Dynamic Characterization of Large Structures and Its Application to Solid Rocket Motor Testing and Launch


10.1615/IntJEnergeticMaterialsChemProp.2025055111
CHARACTERISTICS OF PRESSURE OSCILLATIONS IN LARGE SEGMENTED SOLID ROCKET MOTORS


https://doi.org/10.1016/j.ast.2026.112955
Pressure–thrust oscillation characteristics and amplification mechanisms in a backward-facing step solid rocket motors under self-excited and forced conditions


https://doi.org/10.1063/5.0222294
Effects of Mach number on space-time characteristics of wall pressure fluctuations beneath turbulent boundary layers

https://doi.org/10.4271/2024-26-0459
Fast Coupled Load Analysis through Reanalysis Technique: Formulation and Demonstration on Sample Problems

https://doi.org/10.1049/icp.2024.3064
Modeling and validation of high-speed pneumatic system for interstage separation

https://doi.org/10.17764/1098-4321.60.1.31
Synthesis of a Time History Based on the Sine-on-Random Prediction Methodology Defined in MIL-STD-810 Method 519

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