ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Method of three-dimensional curved stream-surface and its application in external waverider
Received date: 2024-04-07
Revised date: 2024-05-22
Accepted date: 2024-06-03
Online published: 2024-06-14
Supported by
National Natural Science Foundation of China(U21B6003);Project 1912
Using the most phenomenon of common shock wave in hypersonic flow for aerodynamic profile design is one of the important directions of aircraft research. To solve the three-dimensional curved shock flow field more accurately and efficiently, a new inverse design method, called the method of three-dimensional curved stream-surface, is proposed for the design of waverider. The new method discretizes the pre-given three-dimensional curved shock surface into multiple flow surfaces, and calculates the flow field in the curved flow surface according to the aerodynamic parameters of the stream-surface and their derivatives. In this way, the streamline in the calculation process is always in the curved stream-surface. Two shock waves with different three-dimensional characteristics are specified as input to prove the effectiveness of this method. The results show that the wall pressure ratio error is less than 1.07% in the conical flow field and the elliptic curved cone flow field compared with inviscid CFD results. At the same time, this method is applied to the design of waveriders for specified elliptic conical shock. The accuracy of this method for the design of waverider is verified by inviscid CFD simulation, with the maximum wall pressure ratio error being only 0.26% and the calculation time and resources being reduced by about 40% compared with the Local-Turning Osculating Cones Method under the same conditions. Therefore, the method of three-dimensional curved stream-surface can greatly improve the scope and efficiency of the waverider design, and is conducive to the design of the aerodynamic system of hypersonic vehicle.
Kai YANG , Mengfei ZHANG , Chongguang SHI , Yaokun YU , Xiaogang ZHENG , Chengxiang ZHU , Yancheng YOU . Method of three-dimensional curved stream-surface and its application in external waverider[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2025 , 46(2) : 130492 -130492 . DOI: 10.7527/S1000-6893.2024.30492
1 | WANG F M, DING H H, LEI M F. Aerodynamic characteristics research on wide-speed range waverider configuration[J]. Science in China Series E: Technological Sciences, 2009, 52(10): 2903-2910. |
2 | NONWEILER T R F. Aerodynamic problems of manned space vehicles[J]. The Journal of the Royal Aeronautical Society, 1959, 63(585): 521-528. |
3 | O’NEILL M K L, LEWIS M J. Design tradeoffs on scramjet engine integrated hypersonic waverider vehicles[J]. Journal of Aircraft, 1993, 30(6): 943-952. |
4 | CUI K, LI G L, XIAO Y, et al. High-pressure capturing wing configurations[J]. AIAA Journal, 2017, 55(6): 1909-1919. |
5 | CUI K, XIAO Y, XU Y Z, et al. Hypersonic I-shaped aerodynamic configurations[J]. Science China Physics, Mechanics & Astronomy, 2017, 61(2): 024722. |
6 | JONES J G, MOORE K C, PIKE J, et al. A method for designing lifting configurations for high supersonic speeds, using axisymmetric flow fields[J]. Ingenieur-Archiv, 1968, 37(1): 56-72. |
7 | RASMUSSEN M L, JISCHKE M C, DANIEL D C. Experimental forces and moments on cone-derived waveriders for M=3 to 5[J]. Journal of Spacecraft and Rockets, 1982, 19(6): 592-598. |
8 | LIAO J R, ISAAC K M, MILES J B, et al. Navier-Stokes simulation for cone-derived waverider[J]. AIAA Journal, 1992, 30(6): 1521-1528. |
9 | LIN S C, SHEN M C. Navier-Stokes simulation of a cone-derived waverider with multidirectional curvature[J]. AIAA Journal, 1996, 34(8): 1739-1741. |
10 | 王丁, 王江峰, 李龙飞. 基于三维特征线理论的曲面激波流场反设计方法[J]. 空气动力学学报, 2023, 41(4): 11-30. |
WANG D, WANG J F, LI L F. Inverse design method of three-dimensional shocked flow fields based on the theory of three-dimensional characteristic lines[J]. Acta Aerodynamica Sinica, 2023, 41(4): 11-30 (in Chinese). | |
11 | ZUCROW M J, HOFFMAN J D. Gas dynamics[M]. New York: Wiley, 1976. |
12 | JONES K D, SOBIECZKY H, SEEBASS A R, et al. Waverider design for generalized shock geometries[J]. Journal of Spacecraft and Rockets, 1995, 32(6): 957-963. |
13 | SOBIECZKY H, ZORES B, ZHUO W. High speed flow design using the theory of osculating cones and axisymmetric flows[J]. Chinese Journal of Aeronautics, 1999, 12(1):1-8. |
14 | ZHENG X G, HU Z C, LI Y Q, et al. Local-turning osculating cones method for waverider design[J]. AIAA Journal, 2020, 58(8): 3499-3513. |
15 | LIU Z, LIU J, DING F, et al. Novel osculating flowfield methodology for hypersonic waverider vehicles based on variable shock angle[J]. Journal of Aerospace Engineering, 2018, 31(4): 04018043. |
16 | CHAUFFOUR M L, LEWIS M. Corrected shock-based design for waverider geometries[C]∥ 12th AIAA International Space Planes and Hypersonic Systems and Technologies. Reston: AIAA, 2003: 7060. |
17 | CHAUFFOUR M L, LEWIS M. Corrected waverider design for inlet applications[C]∥ 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Reston: AIAA, 2004: 3405. |
18 | LEWIS M J, CHAUFFOUR M L. Shock-based waverider design with pressure gradient corrections and computational simulations[J]. Journal of Aircraft, 2005, 42(5): 1350-1352. |
19 | ZHENG X G, LI Y Q, ZHU C X, et al. Multiple osculating cones’ waverider design method for ruled shock surfaces[J]. AIAA Journal, 2019, 58(2): 854-866. |
20 | HUANG G P, ZUO F Y, QIAO W Y. Design method of internal waverider inlet under non-uniform upstream for inlet/forebody integration[J]. Aerospace Science and Technology, 2018, 74: 160-172. |
21 | 赵玉新, 蓝庆生, 赵一龙. 三维曲面激波反问题的参考平面解法[J]. 推进技术, 2018, 39(11): 2454-2462. |
ZHAO Y X, LAN Q S, ZHAO Y L. Reference plane method for inverse problem of three-dimensional curved shock wave[J]. Journal of Propulsion Technology, 2018, 39(11): 2454-2462 (in Chinese). | |
22 | 赵玉新, 蓝庆生, 赵一龙, 等. 三维超声速压力反问题的特征线求解技术[J]. 推进技术, 2018, 39(10): 2340-2350. |
ZHAO Y X, LAN Q S, ZHAO Y L, et al. A characteristic method for solving three-dimensional supersonic pressure inverse problems[J]. Journal of Propulsion Technology, 2018, 39(10): 2340-2350 (in Chinese). | |
23 | EMANUEL G, M?LDER S. Three-dimensional curved shock theory[J]. Shock Waves, 2022, 32(2): 129-146. |
24 | M?LDER S. Curved shock theory[J]. Shock Waves, 2016, 26(4): 337-353. |
25 | SHI C G, ZHU C X, YOU Y C, et al. Method of curved-shock characteristics with application to inverse design of supersonic flowfields[J]. Journal of Fluid Mechanics, 2021, 920: A36. |
/
〈 |
|
〉 |