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| 封面 |
| 2021,18(3) |
| Abstract(2269) View PDF(2413) |
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| 目录 |
| 2021,18(3) |
| Abstract(2181) View PDF(1975) |
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| 专刊主编介绍 |
| 2021,18(3) |
| Abstract(2314) View PDF(1801) |
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| 专刊序言 |
| 2021,18(3) |
| Abstract(2186) View PDF(1795) |
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| Recent Development of Re-entry Aero-thermal-dynamic Environmental Prediction and Test Technology |
| KANG Tian, LI Ming-hai, LI Chun-li, WANG Wen, ZHOU Lin, WU Lian-jun, LIU Qing-lin |
| 2021,18(3):1-8 |
| Abstract(3532) View PDF(2086) |
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| Engineering Prediction Method of the Vibration Environment for Re-entry Vehicle |
| LI Chun-li, SHI Xian-jie |
| 2021,18(3):9-13 |
| Abstract(3024) View PDF(2037) |
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| Discussion on Prediction Methods of Fluctuating Pressure Environments of Flow Fields Surrounding the Aircraft |
| MA Shi-wei, JIANG Hua-bing |
| 2021,18(3):14-22 |
| Abstract(3330) View PDF(2142) |
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| A HFS Solver for Simulation of Fluctuation Pressure in Compressible Flow |
| ZHOU Lin, SHEN Yi, GE Ren-wei |
| 2021,18(3):23-28 |
| Abstract(2837) View PDF(2027) |
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| Random Vibration Analysis of Free Body Under Fluctuating Pressure Considering Correlation |
| XU Mao, LI Shang-ming, WU Lian-jun |
| 2021,18(3):29-33 |
| Abstract(2792) View PDF(2011) |
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| Numerical Analysis of Random Vibro-acoustic Based on Finite Element Method |
| WU Lian-jun, CHEN Hong-yong |
| 2021,18(3):34-37 |
| Abstract(3446) View PDF(2044) |
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| Random Vibration Response Analysis of Aircraft with Pulsating Pressure Excitation Based on PANDA Platform |
| WANG Ke-ying, HU jie, FAN Xuan-hua, NIU Hong-pan |
| 2021,18(3):38-44 |
| Abstract(2893) View PDF(2134) |
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| Wind Tunnel Test Research on Surface Pressure Fluctuations of a Blunt Cone |
| WANG Wen, JIANG Hua-bin |
| 2021,18(3):45-50 |
| Abstract(3268) View PDF(2049) |
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| Model Flight Test Design to Measure Re-entry Aero-thermal-dynamic Environments |
| KANG Tian, JIANG Hua-bing, SHAN Ji-xiang |
| 2021,18(3):51-56 |
| Abstract(3041) View PDF(2106) |
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| Overall Design and Key Technologies of the Re-entry Environment Flight Test Rocket |
| ONG Yan, LI Hao, XU Xin-yin, SHAN Ji-xiang, ZHAO Ping, ZENG Fei |
| 2021,18(3):57-62 |
| Abstract(2876) View PDF(2117) |
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| Effect of the Attack Angle on the Reentry Warhead Aerodynamic Heating Environment and Structure Thermal Response |
| SHAN Ji-xiang, CHEN Qiang-hong, ZHAO Ping |
| 2021,18(3):63-69 |
| Abstract(2790) View PDF(2043) |
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| The Balancing Rotating Speed Analyses and Trajectory Design of Rolling Tail Rocker Projectile |
| LI Bo, ZHANG Xu, CHEN Qiang-hong, ZHAO Ping, DONG Yan, ZENG Fei |
| 2021,18(3):70-76 |
| Abstract(3207) View PDF(1983) |
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| Design of Multi-channel Weak Signal Conditioning Circuit for Fluctuating Pressure of Rocket Test Platform |
| ZHANG Qi, NIE Fei, ZHANG Cheng, QIAO Gang, LUO Cheng-gang |
| 2021,18(3):77-81 |
| Abstract(3005) View PDF(2036) |
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| The Synchronizing Sample and Data Recovery for Multi-channel Fluctuating Pressure in the Rocket Test Platform |
| ZHANG Cheng, ZHANG Qi, NIE Fei, LUO Cheng-gang, LIU Jing |
| 2021,18(3):82-85 |
| Abstract(2960) View PDF(2030) |
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| The Equivalence of Re-entry Flight Ground Vibration Test |
| SU Bo, ZHANG Gao-nan, SHI Xian-jie |
| 2021,18(3):86-91 |
| Abstract(2899) View PDF(2088) |
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| Experimental Study on Two Points Response Control Technology for Typical Conical Structures |
| ZHOU Tong, HU Jie, OUYANG Zhi-jiang, ZHAO Huai-yun |
| 2021,18(3):92-96 |
| Abstract(3220) View PDF(2010) |
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| The Control Techniques in the Vibro-acoustic Test |
| LIU Qing-lin, WANG Dong-sheng, LI Ming-hai |
| 2021,18(3):97-100 |
| Abstract(3256) View PDF(1972) |
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| The Design of Overloaded Transient Thermal Testing Apparatus to Simulate Re-entry Heating and Testing Techniques |
| WU Song, HU Yu-peng, LI Chong, LU Jia-fu, LU Liang, ZHANG Shuai, CHEN Jun, OU Feng |
| 2021,18(3):101-106 |
| Abstract(3426) View PDF(2087) |
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