To systematically analyze the dynamic characteristics of rocket sled travelling along rail,the three⁃dimensional Eluer⁃Bernouli beam elements were used to discretize the rocket sled system,and the nonlinear contact force model of the slipper⁃rail considering rail irregularity and slipper wear was established by reconstructing the long⁃range irregularity rail,and finally,the nonlinear dynamics equations was solved by Newmark⁃
β
combined with Newton⁃Raphson local iteration method to obtain the numerical solution of dynamic characteristics on rocket sled. Though experimental verification,the results showed that the peak value of the vertical overload to the mass of rocket sled was about 2 700
g
at Mach number of 2 speed;the duty cycle of rocket sled on rail was proportional to forward speed,and the vertical duty cycle of rocket sled was 16% at Mach number of 2 speed;the wear of slippers in high speed section accounted for 84% of the total trajectory wear,and the single contact wear of slipper⁃rail was proportional to the third power of the forward speed.
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references
BEUTLER F J . Precision measurement of supersonic rocket sled velocity:Part Ⅱ [J]. Journal of Jet Propulsion , 2015 , 28 ( 12 ): 809 ⁃ 816 .
LAIRD D J . The investigation of hypervelocity gouging [D]. Dayton,Ohio,USA : Air Force Institute of Technology Air University , 2002 .
HOOSER M , SCHWING A . Validation of dynamic simulation techniques at the holloman high speed test track [R].AIAA 2000 ⁃0155 , 2000 .
王健 . 高速火箭橇⁃轨道系统耦合动力学研究 [D]. 南京 : 南京理工大学 , 2011 .
WANG Jian . The research for coupled dynamics of high speed rocket sled⁃track systems [D]. Nanjing : Nanjing University of Science Technology , 2011 . (in Chinese)
GU Kaixuan , GONG Mingsheng , WANG Lei , et al . Study on full time dynamics simulation of two⁃track rocket sled [J]. Advances in Aeronautical Science and Engineering , 2020 , 11 ( 2 ): 245 ⁃ 250 . (in Chinese)
YANG Zhen , FAN Kun , HU Bing , et al . Study on dynamic load prediction of the supersonic monorail rocket sled [J]. Journal of Ordnance Equipment Engineering , 2019 , 40 ( 3 ): 247 ⁃ 251 . (in Chinese)
FURLOW J S . Parametric dynamic load prediction of a narrow gauge rocket sled [D]. Las Cruces,New Mexico,US : New Mexico State University , 2006 .
LAMBJAMES L . Critical velocities for rocket sled excitation of rail resonance [J]. Johns Hopkins APL Technical Digest , 2000 , 21 ( 3 ): 448 ⁃ 458 .
FANG Ming , SUN Jianhong , YU Yuanyuan , et al . Friction analyses of the rocket sled system [J]. Journal of Aerospace Power , 2017 , 32 ( 11 ): 2769 ⁃ 2776 . (in Chinese)
SUN K , PENG W X , WEI B H , et al . Friction and wear characteristics of 18Ni(300) maraging steel under high⁃speed dry sliding conditions [J]. Materials , 2020 , 13 ( 7 ), 1485 ⁃ 1494 .
WEI Binghui , SUN Kun , WANG Yunpeng , et al . Finite element prediction for friction coefficient of high speed dry sliding [J]. Journal of Xi'an Jiaotong University , 2020 , 54 ( 6 ): 82 : 89 . (in Chinese)
WANG F , LUO G H , YANG X G , et al . Research on modeling and dynamic characteristics of complex coaxial rotor system [J]. Journal of Vibroengineering , 2017 , 19 ( 3 ): 1524 ⁃ 1545 .
ZHAO Xiangwei . Investigation for effects of static eccentricity on dynamic characteristics of squeeze film damper [D]. Nanjing : Nanjing University of Aeronautics and Astronautics , 2018 . (in Chinese)
HOOSER C D . Holloman high speed test track rail alignment criteria [R]. AIAA⁃2000⁃0156 , 2000 .
KEVIN D . Holloman high speed test track design manual [R]. AAC/PA 07⁃13⁃05⁃270, 2005 .
HOOSER M . Simulation of a 10 000 foot per second ground vehicle [R]. AIAA⁃2000⁃2290 , 2000 .
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