ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2023, Vol. 44 ›› Issue (12): 127857-127857.doi: 10.7527/S1000-6893.2022.27857
• Fluid Mechanics and Flight Mechanics • Previous Articles Next Articles
Yongzhou LI1(), Di SUN1, Renhua WANG2, Kunyuan ZHANG3
Received:
2022-07-26
Revised:
2022-08-03
Accepted:
2022-08-26
Online:
2023-06-25
Published:
2022-09-13
Contact:
Yongzhou LI
E-mail:nuaa-2004@126.com
Supported by:
CLC Number:
Yongzhou LI, Di SUN, Renhua WANG, Kunyuan ZHANG. Design of inward turning inlet with controlled Mach number under non-uniform inflow[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(12): 127857-127857.
1 | 蔡伊雯, 金志光, 周建兴, 等. 一种多热力循环组合发动机进气道设计方案[J]. 航空学报, 2020, 41(11): 123745. |
CAI Y W. JIN Z G. ZHOU J X.et al. Design scheme of combined multiple thermodynamic cycle engine inlet[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(11): 123745 (in Chinese). | |
2 | LI Y Q, YOU Y C, HAN W Q, et al. An innovative integration concept for forebody and two-dimensional hypersonic inlet with controllable wall pressure distribution: AIAA-2015-3592[R]. Reston: AIAA, 2015. |
3 | ZHANG L, ZHANG K Y, WANG L. Experimental study of three-dimensional sidewall compression inlet designed on wall Mach number linear distribution curved surface compression system: AIAA-2015-3669[R]. Reston: AIAA, 2015. |
4 | BILLIG F S, JACOBSEN L S. Comparison of planar and axisymmetric flow paths for hydrogen fueled space access vehicle: AIAA-2003-4407[R]. Reston: AIAA, 2003. |
5 | ZHANG K Y. Research progress of hypersonic inlet inverse design based on curved shock compression system: AIAA-2015-3647[R]. Reston: AIAA, 2015. |
6 | 王卫星, 朱婷, 张仁涛, 等. 高超声速内转式进气道型面流场重构[J]. 航空学报,2020,41(3): 123493. |
WANG W X, ZHU T, ZHANG R T . et al. Flow field reconstruction of hypersonic inward turning inlet based on configurations[J]. Acta Aeronautica et Astronautica Sinica,2020, 41(3): 123493 (in Chinese). | |
7 | 张航, 孙姝, 黄河峡, 等. 高超声速双模块内转式进气道的流动特性研究-PartⅠ:设计状态[J]. 推进技术, 2022,43(7):101-109. |
ZHANG H, SUN S, HUANG H X, et al. Flowfield of hypersonic bimodal inward-turning inlet-part i: design point[J]. Journal of Propulsion Technology, 2022, 43(7):101-109 (in Chinese). | |
8 | 蔡泽君, 胡占仓, 余联郴, 等. XTER内收缩组合进气道设计理念及气动特性[J]. 空气动力学学报, 2022, 40(1): 218-231. |
CAI Z J, HU Z C, YU L C, et al. Design concept and aerodynamic characteristics of XTER TBCC inlet[J]. Acta Aerodynamica Sinica, 2022, 40(1): 218-231 (in Chinese). | |
9 | BOYCE R, GERARD S, PAULL A. The HyShot scramjet flight experiment-flight data and CFD calculations compared: AIAA-2003-7029[R]. Reston: AIAA, 2003. |
10 | MÖLDER S, SZPIRO J. Busemman inlet for hypersonic speeds[J]. Journal of Spacecraft and Rockets, 1966, 3(8): 1303-1304. |
11 | SMART M K. Design of three-dimensional hypersonic inlets with rectangular-to-elliptical shape transition[J]. Journal of Power and Propulsion, 1999, 15(3): 408-416. |
12 | MATTHEWS A J, JONES T V. Design and test of a modular waverider hypersonic intake[J]. Journal of Propulsion and Power, 2006, 22(4): 913-920. |
13 | 尤延铖, 梁德旺. 基于内乘波概念的三维变截面高超声速进气道[J]. 中国科学E辑: 技术科学, 2009, 39(8): 1483-1494. |
YOU Y C, LIANG D W. Design concept of three dimensional section controllable internal waverider hypersonic inlet[J]. Science in China Series E:Technological Sciences, 2009, 39(8): 1483-1494 (in Chinese). | |
14 | YUE L J, XIAO Y B, CHEN L H, et al. Design of base flow for streamline-traced hypersonic inlet: AIAA-2009-7422[R]. Reston: AIAA, 2009. |
15 | 南向军,张堃元,金志光,等. 矩形转圆形高超声速内收缩进气道数值及实验研究[J]. 航空学报, 2011, 32(6): 988-996. |
NAN X J, ZHANG K Y, JIN Z G, et al. Numerical and experimental investigation of hypersonic inward turning inlets with rectangular to circular shape transition[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(6): 988-996 (in Chinese). | |
16 | 李永洲,张堃元,南向军. 基于马赫数分布规律可控概念的高超声速内收缩进气道设计[J]. 航空动力学报, 2012, 27(11): 2484-2491. |
LI Y Z, ZHANG K Y, NAN X J. Design concept of controllable Mach number distribution hypersonic inward turning inlets[J]. Journal of Aerospace Power, 2012, 27(11): 2484-2491 (in Chinese). | |
17 | SOBIECZKY H, ZORES B, WANG Z. High speed flow design using the theory of osculating cones and axisymmetric flows[J]. Chinese Journal of Aeronautics, 1999, 12(1): 1-8. |
18 | 乔文友, 余安远. 内转式进气道与飞行器前体的一体化设计综述[J]. 实验流体力学, 2019, 33(3): 43-59. |
QIAO W J, YU A Y. Overview on integrated design of inward-turning inlet with aircraft forebody[J]. Journal of Experiments in Fluid Mechanics, 2019, 33(3):43-59 (in Chinese). | |
19 | 张文浩, 柳军, 丁峰. 内转式进气道/冯·卡门乘波体一体化设计方法[J]. 航空学报, 2020, 41(3): 123502. |
ZHANG W H, LIU J, DING F. Integrated design method of inward turning inlet /Von Karman waverider[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(3): 123502 (in Chinese). | |
20 | 贺旭照, 卫锋, 刘福军, 等. 最小波阻锥导乘波体和三维内转式进气道一体化设计[J]. 空气动力学学报, 2022, 40(1): 77-83. |
HE X Z, WEI F LIU F J, et al. Integrated design of minimal wave drag cone-derived waveriders and three-dimensional inward turning inlets[J]. Acta Aerodynamica Sinica, 40(1): 77-83 (in Chinese). | |
21 | LAWING P L, JOHNSON C B. Inlet boundary-layer shapes on four aircraft forebodies at Mach 6[J]. Journal of Aircraft, 1978, 15(1): 62-63. |
22 | JOHNSON C B, LAWING P L. Mach 6 flow field survey at the engine inlet of a research airplane[J]. Journal of Aircraft, 1977, 14(4): 412-414. |
23 | EKOTO I W, BOWERSOX D W B. Planar measurements of supersonic boundary layers with curvature driven pressure gradients: AIAA-2007-1137[R]. Reston: AIAA, 2007. |
24 | LEWIS M J, ASTINGS D E. Application of compound compressible flow to nonuniformities in hypersonic propulsion systems[J]. Journal of Propulsion and Power, 1989, 5(5):626-634. |
25 | 张堃元, 萧旭东, 徐辉. 高超侧压式进气道参数分析及试验研究[J]. 推进技术, 1995, 16(6): 20-25. |
ZHANG K Y, XIAO X D, XU H. Parametric analysis and experimental investigation on sidewall compression inlet[J]. Journal of Propulsion Technology, 1995, 16(6): 20-25 (in Chinese). | |
26 | 高雄. 超声速非均匀流模拟方法研究[D]. 南京:南京航空航天大学, 2009: 21-39. |
GAO X. Investigation of supersonic non-uniform flow simulation method[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009: 21-39 (in Chinese). | |
27 | 方兴军. 控制出口速度分布的超声速内流通道反设计[D]. 南京:南京航空航天大学,2012. |
FANG X J. inverse design of supersonic internal flow path based on given outflow velocity profile[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012 (in Chinese). | |
28 | 周航, 金志光. 非均匀来流下三维激波反问题的微元密切轴对称解法[J]. 航空学报, 2020, 41(12): 124035. |
ZHOU H, JIN Z G. Micro osculating axisymmetric flow method for 3D shock wave design under nonuniform flows[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(12): 124035 (in Chinese). | |
29 | 李永洲, 张堃元. 基于马赫数分布可控曲面外/内锥形基准流场的前体/进气道一体化设计[J]. 航空学报,2015,36(1):289-301. |
LI Y Z, ZHANU K Y. Integrated design of forebody and inlet based on external and internal conical basic flow field with controlled Mach number distribution surface[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1): 289-301 (in Chinese). | |
30 | DRAYNA T W, NOMPELIS I, CANDLER G V. Hypersonic inward turning inlets: design and optimization: AIAA-2006-297[R]. Reston: AIAA, 2006. |
31 | 李永洲, 张堃元, 孙迪. 马赫数可控的方转圆高超声速内收缩进气道试验研究[J]. 航空学报,2016, 37(10): 2970-2979. |
LI Y Z, ZHANG K Y, SUN D. Experimental investigation on a hypersonic inward turning inlet of rectangular-to-circular shape with controlled Mach number distribution[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(10): 2970-2979 (in Chinese). | |
32 | 王翼. 高超声速进气道启动问题研究[D]. 长沙:国防科学技术大学研究生院, 2008: 27-30. |
WANG Y. Investigation on the starting characteristics of hypersonic inlet[D]. Changsha: Graduate School of National University of Defense Technology, 2008: 27-30 (in Chinese). |
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Total visits: 6658907 Today visits: 1341