宽速域高压捕获翼气动构型及其跨声速气动特性

doi:10.7527/S1000-6893.2025.32102

Abstract

Abstract:

In recent decades， wide-speed-range aircraft with hypersonic cruise capability have garnered significant attention and emerged as a prominent research focus worldwide. However， a wider flight velocity range poses significant challenges to aerodynamic configuration design. To effectively overcome the trade-off between lift-to-drag ratio and volumetric efficiency， we propose a novel aerodynamic configuration with high volumetric capacity based on the high-pressure capturing wing concept. Numerical simulations demonstrate that this configuration achieves a maximum lift-to-drag ratio of 5.89 at Mach number 6.0， representing an improvement of over 18% compared to a reference configuration without the high-pressure capturing wing. Furthermore， numerical simulations and analyses were conducted focusing on two typical transonic conditions at Mach number 0.8 and 1.2. The results demonstrate that compared to the reference configuration， the new high-pressure capturing wing configuration exhibits increased lift and drag coefficients to varying degrees under both transonic conditions. Although this comes with some degradation in lift-to-drag ratio， the shift of the aerodynamic center is significantly reduced across the wide speed range. Specifically， the relative shift of the aerodynamic center is reduced by 11.1% in the transonic regime and by 49.9% across the transonic-to-hypersonic regime. Further analysis reveals that this reduction in aerodynamic center shift is primarily attributed to the coupling effects between the additional wing surface and the fuselage.

Key words: wide speed range, high-pressure capturing wing, aerodynamic configurations, computational fluid dynamics, transonic speed

CLC Number:

V211.3

Kai CUI, Zesen WANG, Yao XIAO, Zhongwei TIAN, Guangli LI, Siyuan CHANG. A novel wide-speed-range configuration based on high-pressure capturing wing concept and its transonic aerodynamic characteristics[J]. Acta Aeronautica et Astronautica Sinica, 2026, 47(1): 632102.

Figures/Tables 31

Fig.1

Fig.2

Fig.3

Fig.4

Fig.5

Table 1

Fig.6

Fig.7

Table 2

Fig.8

Fig.9

Fig.10

Fig.11

Fig.12

Fig.13

Fig.14

Fig.15

Fig.16

Fig.17

Fig.18

Fig.19

Fig.20

Fig.21

Fig.22

Table 3

Fig.23

Fig.24

Fig.25

Fig.26

Fig.27

Fig.28

References 35

[1]	SZIROCZAK D， SMITH H. A review of design issues specific to hypersonic flight vehicles［J］. Progress in Aerospace Sciences， 2016， 84： 1-28.
[2]	DREW J. Lockheed holding fast on SR-72 plan［J］. Flight International， 2016， 189（5531）： 8.
[3]	张灿，林旭斌，胡冬冬，等. 2018年国外高超声速飞行器技术发展综述［J］. 飞航导弹， 2019（2）： 1-5， 15.
	ZHANG C， LIN X B， HU D D， et al. A review of foreign hypersonic vehicle technology developments in 2018［J］. Aerodynamic Missile Journal， 2019（2）： 1-5， 15 （in Chinese）.
[4]	STEELANT J， VAN DUIGN M. Structural analysis of the LAPCAT-MR2 waverider based vehicle［C］∥17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston： AIAA， 2011.
[5]	STEELANT J， VARVILL R， WALTON C， et al. Achievements obtained for sustained hypersonic flight within the LAPCAT-Ⅱ project［C］∥20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston： AIAA， 2015.
[6]	VAN BRUMMEN S， PEZZELLA G， ANDREUTTI G， et al. Aerodynamic design analysis of the HEXAFLY-INT hypersonic glider［C］∥20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference， Reston： AIAA， 2015.
[7]	STEELANT J， VILLACE V， KALLENBACH A， et al. Flight testing designs in HEXAFLY-INT for high-speed transportation［J］. Proceedings of HiSST， 2018.
[8]	RODI P. Geometrical relationships for osculating cones and osculating flowfield waveriders［C］∥49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston： AIAA， 2011.
[9]	RODI P. Vortex lift waverider configurations［C］∥50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston： AIAA， 2012.
[10]	刘传振，白鹏，陈冰雁. 双后掠乘波体设计及性能优势分析［J］. 航空学报， 2017， 38（6）： 120808.
	LIU C Z， BAI P， CHEN B Y. Design and property advantages analysis of double swept waverider［J］. Acta Aeronautica et Astronautica Sinica， 2017， 38（6）： 120808 （in Chinese）.
[11]	刘传振，刘强，白鹏，等. 涡波效应宽速域气动外形设计［J］. 航空学报， 2018， 39（7）： 121824.
	LIU C Z， LIU Q， BAI P， et al. Aerodynamic shape design integrating vortex and shock effects for width-velocity-range［J］. Acta Aeronautica et Astronautica Sinica， 2018， 39（7）： 121824 （in Chinese）.
[12]	LIU C Z， MENG X F， LIU J， et al. Experimental investigation for subsonic， transonic， and supersonic performances of double-swept waverider［J］. AIAA Journal， 2023， 61（10）： 4247-4258.
[13]	LIU C Z， LIU R J， MENG X F， et al. Experimental investigation on off-design performances of double-swept waverider［J］. AIAA Journal， 2023， 61（4）： 1596-1607.
[14]	刘超宇，屈峰，李杰奇，等. 涡波一体乘波飞行器宽速域气动优化设计研究［J］. 力学学报， 2023， 55（1）： 70-83.
	LIU C Y， QU F， LI J Q， et al. Aerodynamic optimization design of the vortex-shock integrated waverider in wide speed range［J］. Chinese Journal of Theoretical and Applied Mechanics， 2023， 55（1）： 70-83 （in Chinese）.
[15]	UENO A， SUZUKI K. Two-dimensional shape optimization of hypersonic vehicles considering transonic aerodynamic performance［J］. Transactions of the Japan Society for Aeronautical and Space Sciences， 2009， 52（176）： 65-73.
[16]	LIU F， HAN Z H， ZHANG Y， et al. Surrogate-based aerodynamic shape optimization of hypersonic flows considering transonic performance［J］. Aerospace Science and Technology， 2019， 93： 105345.
[17]	陈树生，张兆康，李金平，等. 一种宽速域乘波三角翼气动布局设计［J］. 航空学报， 2023， 44（23）： 128441.
	CHEN S S， ZHANG Z K， LI J P， et al. Wide-speed aerodynamic layout adopting waverider-delta wing［J］. Acta Aeronautica et Astronautica Sinica， 2023， 44（23）： 128441 （in Chinese）.
[18]	刘文，郭帅旗，刘洋，等. 乘波体设计与优化研究进展——从高超声速至宽速域［J］. 力学学报， 2024， 56（6）： 1655-1677.
	LIU W， GUO S Q， LIU Y， et al. Advances in design and optimization of waverider—From hypersonic to wide-speed range［J］. Chinese Journal of Theoretical and Applied Mechanics， 2024， 56（6）： 1655-1677 （in Chinese）.
[19]	TAKAHASHI T T， GRIFFIN J A， GRANDHI R V. A review of high-speed aircraft stability and control challenges［C］∥AIAA Aviation 2023 Forum. Reston： AIAA， 2023.
[20]	HEFFLEY R K， JEWELL W F. Aircraft handling qualities data：AD-A277031［R］. Washington， D.C.： NASA， 1972.
[21]	肖尧，崔凯，李广利，等. 高压捕获翼双翼构型宽速域气动性能研究［J］. 气体物理， 2023， 8（5）： 54-60.
	XIAO Y， CUI K， LI G L， et al. Research on aerodynamic performance of high-pressure capturing wing with bi-wing configuration in wide-speed range［J］. Physics of Gases， 2023， 8（5）： 54-60 （in Chinese）.
[22]	崔凯，李广利，胡守超，等. 高速飞行器高压捕获翼气动布局概念研究［J］. 中国科学：物理学力学天文学， 2013， 43（5）： 652-661.
	CUI K， LI G L， HU S C， et al. Conceptual studies of the high pressure zone capture wing configuration for high speed air vehicles［J］. Scientia Sinica Physica， Mechanica and Astronomica， 2013， 43（5）： 652-661 （in Chinese）.
[23]	CUI K， LI G L， XIAO Y， et al. High-pressure capturing wing configurations［J］. AIAA Journal， 2017， 55（6）： 1909-1919.
[24]	李广利，崔凯，肖尧，等. 高压捕获翼前缘型线优化和分析［J］. 力学学报， 2016， 48（4）： 877-885.
	LI G L， CUI K， XIAO Y， et al. Leading edge optimization and parameter analysis of high pressure capturing wings［J］. Chinese Journal of Theoretical and Applied Mechanics， 2016， 48（4）： 877-885 （in Chinese）.
[25]	常思源，肖尧，李广利，等. 翼反角对高压捕获翼构型高超气动特性的影响［J］. 航空学报， 2023， 44（8）： 127349.
	CHANG S Y， XIAO Y， LI G L， et al. Effect of wing dihedral and anhedral angles on hypersonic aerodynamic characteristics of high-pressure capturing wing configuration ［J］. Acta Aeronautica et Astronautica Sinica， 2023， 44（8）： 127349 （in Chinese）.
[26]	WANG Y L， WEI Y J， WANG C， et al. Theoretical and numerical simulation study on aerodynamics of V configuration high-pressure capture wing （HCW-V）［J］. Physics of Fluids， 2022， 34（8）： 086106.
[27]	GUO J， LEI J M， ZHANG L Y， et al. Drag reduction and lift enhancement mechanism induced by a novel combinational spike and high-pressure capturing wing concept in hypersonic flows［J］. Physics of Fluids， 2025， 37（2）： 026135.
[28]	XI X Z， LI G L， WANG H X， et al. Numerical investigation of the influence of fuselage corner bluntness on a high-pressure capturing wing configuration［J］. Journal of Aerospace Engineering， 2025， 38（2）： 04024120.
[29]	崔凯，杨靖，常思源，等. 基于POD和代理模型的高压捕获翼表面流场快速预测方法［J］. 力学学报， 2025， 57（4）： 883-894.
	CUI K， YANG J， CHANG S Y， et al. Rapid prediction method for high-pressure capturing wing surface flow field based on proper orthogonal decomposition and surrogate model［J］. Chinese Journal of Theoretical and Applied Mechanics， 2025， 57（4）： 883-894 （in Chinese）.
[30]	王浩祥，李广利，徐应洲，等. 高压捕获翼构型跨声速流动特性初步研究［J］. 空气动力学学报， 2020， 38（3）： 441-447.
	WANG H X， LI G L， XU Y Z， et al. Preliminary study on transonic flow characteristics of a high-pressure capturing wing configuration［J］. Acta Aerodynamica Sinica， 2020， 38（3）： 441-447 （in Chinese）.
[31]	王浩祥，李广利，杨靖，等. 高压捕获翼构型亚跨超流动特性数值研究［J］. 力学学报， 2021， 53（11）： 3056-3070.
	WANG H X， LI G L， YANG J， et al. Numerical study on flow characteristics of high-pressure capturing wing configuration at subsonic， transonic and supersonic regime［J］. Chinese Journal of Theoretical and Applied Mechanics， 2021， 53（11）： 3056-3070 （in Chinese）.
[32]	LEYMAN C. Case study by aerospatiale and british aerospace on the concorde［M］. Reston： AIAA， 1980： 5-11.
[33]	APROVITOLA A， DYBLENKO O， PEZZELLA G， et al. Aerodynamic analysis of a supersonic transport aircraft at low and high speed flow conditions［J］. Aerospace， 2022， 9（8）： 411.
[34]	王浩祥. 高压捕获翼构型宽速域气动特性数值研究［D］. 北京：中国科学院力学研究所， 2023： 46-54.
	WANG H X. Numerical study on aerodynamic characteristics of high-pressure capturing wing configuration in wide speed range［D］. Beijing： Institute of Mechanics， Chinese Academy of Sciences， 2023： 46-54 （in Chinese）.
[35]	SLATER J W. NPARC alliance verification and validation archive： ONERA M6 wing［EB/OL］. （2021-02-10）［2025-05-26］.

Ma	系数	粗网格	中等网格	细网格
0.8	C_L	0.555	0.552	0.551
	C_D	0.071 0	0.073 1	0.073 8
	C_my	-0.321	-0.318	-0.317
1.2	C_L	0.600	0.594	0.593
	C_D	0.097 7	0.100	0.100
	C_my	-0.383	-0.379	-0.378

Ma	H/km	Re/10⁸	α/（°）
0.8	12	1.55	-4， 0， 4， 6， 8，
1.2	12	2.33	12， 16

Ma	X _ac
Ma	Ref构型	HCT构型
0.8	0.578 7	0.559 6
1.2	0.621 8	0.597 9
6	0.582 5	0.578 2

A novel wide-speed-range configuration based on high-pressure capturing wing concept and its transonic aerodynamic characteristics

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

Figures/Tables 31

References 35

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Xiaofeng YANG, Xingkao CAI, Lei LIU, Dong WEI, Guangming XIAO, Yanxia DU, Yewei GUI. Coupling simulation of aircraft aerothermodynamics regulated by gradient characteristics of thermal protection structure and its experimental verification [J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(9): 130888-130888.
[2]	Binwen WANG, Qiaozhi SONG, Haoyu CHEN. Body freedom flutter ground test of flying wing aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(21): 532758-532758.
[3]	Liwen ZHANG, Zhonghua HAN, Keshi ZHANG, Ke SONG, Wenping SONG. High-fidelity numerical simulation of near-/mid-field sonic boom propagation using a space-marching method for supersonic civil aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(20): 531935-531935.
[4]	Tingyu GUO, Ming YAN, Chunlei XIE. Aerodynamic characteristics of aggregation-separation aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(S1): 730596-730596.
[5]	Qi LIU, Yongjie SHI, Zhiyuan HU, Guohua XU. Parameter effects analysis on aerodynamic and aeroacoustic characteristics of coaxial rigid rotor [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 528856-528856.
[6]	Jianheng JI, Zun CAI, Taiyu WANG, Mingbo SUN, Zhenguo WANG. Flow and combustion process for wide speed range scramjet: Review [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 28696-028696.
[7]	Chengjun SHAN, Tianyu GONG, Lizhe YI, Haohui YANG, Yaosong LONG. High-efficiency and high-reliability sonic boom/aerodynamic multidisciplinary optimization method for supersonic civil aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(24): 630573-630573.
[8]	Mingqi LIU, Zhonghua HAN, Tao DU, Chenzhou XU, Han ZENG, Keshi ZHANG, Wenping SONG. Optimal control efficiency characteristics and wide-speed-range aerodynamic design optimization method for grid fins of launch vehicle [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(20): 129887-129887.
[9]	Li LI, Yihua LIANG, Yong YANG, Junsheng WU. WiseCFD V2023: A software framework with open architecture to support verification and validation and credibility assessment of CFD software [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(20): 630440-630440.
[10]	Fengxia LU, Kun WEI, Chunlei WANG, Heyun BAO, Rupeng ZHU. Accessibility of metal particles in three-phase flow of helicopter intermediate gearbox [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 128524-128524.
[11]	Jiong REN, Gang WANG, Guodong HU, Xiaolu SHI. Adaptive finite volume method with Walsh basis functions [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 127444-127444.
[12]	Siyuan CHANG, Yao XIAO, Guangli LI, Zhongwei TIAN, Kaikai ZHANG, Kai CUI. Effect of wing dihedral and anhedral angles on hypersonic aerodynamic characteristics of high-pressure capturing wing configuration [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 127349-127349.
[13]	Haoxiang WANG, Yao XIAO, Kaikai ZHANG, Guangli LI, Siyuan CHANG, Zhongwei TIAN, Kai CUI. Effect of body trailing edge shape on subsonic flow characteristics of high-pressure capturing wing configuration [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127215-127215.
[14]	Wenbo CAO, Yilang LIU, Weiwei ZHANG. Accelerated convergence method for fluid dynamics solvers based on reduced⁃order model and gradient optimization [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127090-127090.
[15]	Shijun SUN, Xiaolong LI, Yanming LIU, Jianhua WANG, Songtao WANG. Influence of wide-speed-range inflow on aerodynamic performance of supersonic through-flow fan cascade [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(21): 528523-528523.