Regression rate response in spin-stabilized solid fuel ramjets

AM Tahsini - Journal of Mechanics, 2020 - academic.oup.com
The regression rate of the solid fuel in the spinning solid fuel ramjet is investigated here
using numerical simulations. The finite volume solver of the reacting turbulent flow is …

Mechanism of Influence of High‐Speed Self‐Spin on Ignition Transients for a Solid Rocket Motor: a Numerical Simulation

D Guan, S Li, X Sui, N Wang - Propellants, Explosives …, 2020 - Wiley Online Library
High‐speed self‐spin is one of extreme working conditions that alters ignition internal
ballistic performance and can induce ignition abnormalities. To demonstrate the studies on …

Effects of high-speed spin on the reacting flow of drag reduction equipment under rapid depressurization

S Zhou, Y Yu - Applied Thermal Engineering, 2022 - Elsevier
The drag reduction equipment (DRE) suffers dual environmental stress of high-speed spin
and rapid depressurization during the launching process, disturbing the projectile intensely …

Characteristics of the Reacting Flow for the Base‐Bleed Projectile under Dual Stress

S Zhou, Y Yu, Z Ye, L Ma - Propellants, Explosives …, 2021 - Wiley Online Library
While the base‐bleed projectile (BBP) is ejected from the muzzle, high‐speed rotation and
rapid depressurization in the combustion chamber bring much initial disturbance to the BBP …

بررسی تجربی اثر اسپین بر نرخ سوزش پیشرانه ی کامپوزیت دارای ذرات آلومینیوم

محمدی, فراهانی, محمد, مسعود - مجله ی مهندسی مکانیک شریف, 2020‎ - sjme.journals.sharif.edu
این نوشتار به بررسی تجربی اثر شتاب بر نرخ سوزش یک پیشرانه‌ی جامد کامپوزیتی بر
پایه‌ی H‌T‌P‌B دارای ذرات آلومینیوم به‌عنوان یکی از عوامل تعیین‌کننده‌ی فشار محفظه می‌پردازد …

Clustering Analysis on Internal Flow Field of a Spinning Solid Rocket Motor Nozzle

L Sun, F Bao, W Hui, Y Liu, J Sui - 2017 9th International …, 2017 - ieeexplore.ieee.org
Clustering analysis was conducted on a solid rocket motor nozzle to investigate its internal
flow field response under spinning condition. A Reynolds stress model and enhanced wall …

[引用][C] 基于统计学的旋转火箭发动机喷管热结构分析

孙林, 阎海生, 鲍福廷 - 固体火箭技术, 2015

[引用][C] 旋转发动机燃烧室头部气-固两相流场结构分析

冯喜平, 赵胜海, 李进贤, 唐金兰 - 计算机仿真, 2010

[引用][C] 旋转固体火箭发动机喷管热结构分析

孙林, 鲍福廷, 时伟 - 航空计算技术, 2014

[引用][C] Ignition Time Delay in Swirling Supersonic Flow Combustion

AM Tahsini - International Journal of Aerospace and Mechanical …, 2012