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| 封面 |
| | 2021,18(3) |
| | Abstract(1640) View PDF(1817) |
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| 目录 |
| | 2021,18(3) |
| | Abstract(1561) View PDF(1530) |
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| 专刊主编介绍 |
| | 2021,18(3) |
| | Abstract(1635) View PDF(1360) |
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| 专刊序言 |
| | 2021,18(3) |
| | Abstract(1555) View PDF(1360) |
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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(2691) View PDF(1577) |
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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(2309) View PDF(1560) |
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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(2479) View PDF(1627) |
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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(2186) View PDF(1545) |
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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(2120) View PDF(1535) |
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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(2647) View PDF(1578) |
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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(2241) View PDF(1622) |
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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(2465) View PDF(1547) |
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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(2380) View PDF(1659) |
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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(2182) View PDF(1604) |
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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(2113) View PDF(1545) |
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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(2377) View PDF(1548) |
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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(2308) View PDF(1543) |
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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(2291) View PDF(1584) |
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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(2208) View PDF(1630) |
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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(2432) View PDF(1543) |
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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(2409) View PDF(1526) |
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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(2512) View PDF(1606) |
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