| Citation: | Cao Deyi, Lee Chunhian. Optimal design of nozzle for hypersonic vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10): 1162-1165. (in Chinese)
|
|
[1] Park H K. Model of an aero-space plane based on an idealized cone-derived waverider forebody . PH.D. Thesis, University of Oklahoma, 1990 [2] O-Neill M K L. Optimized scramjet engine integration on a waverider airframe . PhD thesis, University of Maryland, 1992 [3] Takashima N. Optimization of waverider-based hypersonic vehicle designs .MPhD thesis, University of Maryland, 1997 [4] 陈兵, 徐旭, 蔡国飙. 二维超燃冲压发动机尾喷管优化设计[J]. 推进技术, 2002, 23(5): 433-437 Chen Bing, Xu Xu, Cai Guobiao. Optimization design of two dimensional scramjet nozzle based on N-S equations [J]. Journal of Propulsion Technology, 2002, 23(5): 433-437(in Chinese) [5] Javaid K H, Serghides V C. Thrust-matching requirements for the concept design of hypersonic waverider vehicles [J]. J Aircraft, 2005, 42(4): 1055-1064 [6] Edwards C L Q, Small W J, Weidner J P. Studies of scramjet/airframe integration techniques for hypersonic aircraft . AIAA 75-2581, 1975 [7] Shapiro A H. The dynamics and thermodynamics of compressible fluid flow [M]. Vol.1. New York: McGraw- Hill Book Co, 1953 [8] 周明, 孙树栋. 遗传算法原理及应用[M]. 北京:国防工业出版社, 1999 Zhou Ming, Sun Shudong. Genetic algorithms: theory and applications [M]. Beijing: National Defense Industry Press, 1999(in Chinese) [9] Eckert E R G. Engineering relations for heat transfer and friction in high-velocity laminar and turbulent boundary-layer flow over surfaces with constant pressure and temperature [J]. Trans ASME, 1956, 78: 1273-1284 [10] Zheng B, Lee C H. The effects of limiters on high resolution computations of hypersonic flows over bodies with complex shapes [J]. Comm Nonlin Sci Numer Simul, 1998, 3(2): 82-87
|
| [1] | LIU Y S，TANG X M，REN X M. Prediction of aircraft surface trajectory based on the GRU-IKF model with attention mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（3）：1028-1036 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0164. |
| [2] | HE Huaiqing, SHI Xiaoshuang, LIU Haohan, HUI Kanghua. Multi-flight Trajectory in Terminal Area Based on Improved Spatio-temporal Model Forecasting Method[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0540 |
| [3] | YAN P，LI Q，HUANG X，et al. Friction and heat flux prediction of lift body under different gas models and slip boundary models[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（4）：1277-1291 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0209. |
| [4] | TANG X W，DING Y，ZHANG S R，et al. Taxi-in time prediction of arrival flight[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（7）：2218-2224 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0625. |
| [5] | SHI Qingyan, ZHAO Wantong, HAN Ping. GTA-Seq2Seq multi-step 4D trajectory prediction model based on spatio-temporal feature extraction[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0679 |
| [6] | LIU X，WANG Z Y，WANG X Y. Optimization three-vector-based model predictive current control for permanent magnet toroidal motor[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3297-3309 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0833. |
| [7] | FANG Y F，WU D Y，LIU T，et al. Model predictive current control of asynchronous motor in rolling mill based on sliding mode theory[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3382-3390 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0576. |
| [8] | HE Xueli, WANG Lijing, ZHAN Xi, MIAO Chongchong. Quantitative Real-time Prediction model of Workload in Aircraft Design Phase[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0279 |
| [9] | LIU X，WANG Z Y，WANG X Y. Model-free predictive current control for permanent magnet toroidal motor with extended state observer[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（4）：1085-1096 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0495. |
| [10] | WAN B，SU X C，WANG J，et al. A precise landing control method based on model predictive control algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（4）：1197-1207 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0383. |
| [11] | GE Jian-hao, GUO Jie, WANG Hao-ning, ZHANG Bao-chao, WAN Yang-yang, TANG Sheng-jing. Adaptive model predictive control for hypersonic morphing gliding vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0081 |
| [12] | DING Jianli, LIU Hu, CAO Weidong. Quantitative model of uncertainty for prediction of flight transit time[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0445 |
| [13] | LIU Y H，HUANG Y，TAN H，et al. On-line prediction method of wing flexible baseline based on autoregressive model[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3426-3433 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0865. |
| [14] | LYU Z Y，NIE X Y，ZHAO A B. Prediction of wing aerodynamic coefficient based on CNN[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（3）：674-680 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0276. |
| [15] | LI J X，DING H B，WANG C，et al. A new overreading model for wet gas vortex metering considering entrained droplet flow parameters[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：815-824 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0364. |
| [16] | LIU F，WANG Z，DAI Y Y，et al. A robust adaptive filtering algorithm based on predicted residuals in integrated navigation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（6）：1301-1310 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0460. |
| [17] | XU Lingliang, CHEN Guiming, LI Qiaoyang. Ultra-local model-free speed predictive control based on ESO for PMSM[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2204-2214. doi: 10.13700/j.bh.1001-5965.2021.0085 |
| [18] | CHEN Bin, LIU Yue, LI Qingzhen, DING Yu, WANG Liwen. Runway temperature hybrid prediction based on MFOA-KELM residual correction under ice and snow[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2153-2164. doi: 10.13700/j.bh.1001-5965.2021.0646 |
| [19] | WANG Tao, ZHANG Wanxin, LI Meng, BU Xueqin, ZHANG Chen, WANG Hailiang. Performance analysis of skin temperature prediction model combining Smith's thermoregulation model with Tanabe model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2482-2493. doi: 10.13700/j.bh.1001-5965.2021.0143 |
| [20] | LIU Qianqian, LIU Yushan, WEN Yeting, HE Jie, LI Xiao, BI Daqiang. Short-term load forecasting method based on PCC-LSTM model[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2529-2536. doi: 10.13700/j.bh.1001-5965.2021.0145 |
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
Liu Wei, Meng Xin, Zheng Jianhuaet al. Multi-machine scheduling problem with multi-time windows: model and algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(3): 330-333. (in Chinese)
DownLoad: