Requirement analyses and optimized design of wing/airfoil for aerospace vehicles

LUO Jinling; LONG Shuangli; TANG Jibin; HAN Zhonghua; ZHANG Yang

doi:10.7638/kqdlxxb-2021.0237

English Version Journal Login

您当前的位置：

首页 >

文章列表页 >

Requirement analyses and optimized design of wing/airfoil for aerospace vehicles

更新时间：2026-05-28

- Requirement analyses and optimized design of wing/airfoil for aerospace vehicles
- Vol. 39, Issue 6, Pages: 101-110(2021)
- 作者机构：
  
  1. 北京空天技术研究所,北京,100074
  2. 西北工业大学翼型、叶栅空气动力学国家级重点实验室,西安,710072
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2021.0237
  CLC： V224
- Published：2021
- 稿件说明：
移动端阅览
罗金玲, 龙双丽, 汤继斌, 等. 空天飞行器机翼/翼型的需求分析及应用[J]. 空气动力学学报, 2021, 39(6): 101−110.

LUO Jinling, LONG Shuangli, TANG Jibin, et al. Requirement analyses and optimized design of wing/airfoil for aerospace vehicles[J]. 2021, 39(6): 101-110.
罗金玲, 龙双丽, 汤继斌, 等. 空天飞行器机翼/翼型的需求分析及应用[J]. 空气动力学学报, 2021, 39(6): 101−110. DOI： 10.7638/kqdlxxb-2021.0237

LUO Jinling, LONG Shuangli, TANG Jibin, et al. Requirement analyses and optimized design of wing/airfoil for aerospace vehicles[J]. 2021, 39(6): 101-110. DOI： 10.7638/kqdlxxb-2021.0237.

摘要

空天飞行器飞行空域大，速域宽，经历亚/跨/超/高超声速飞行，气动特性变化大，传统翼型难以同时满足低速、高速时的设计要求，给机翼/翼型设计提出了新的挑战。本文围绕飞行环境特点，分析了低速高升力与高速高升阻比、升重匹配、结构热防护等设计要求，提出了空天飞行器对机翼/翼型设计的新需求。基于一种新的宽速域翼型，采用数值模拟方法，开展三维流动下翼型与机翼平面形状的一体化优化设计，获得了一种翼型沿展向变化的新机翼，相对优化前，低速时机翼产生的升力效率提高了36.3%，超声速和高超声速升重平衡升阻比分别提高了33.4%和12.9%，新机翼能更好地兼顾低速、跨声速、超声速和高超声速气动性能的要求。将新机翼应用于典型空天飞行器，再通过全机气动外形优化设计，进一步提高了宽速域飞行时升重平衡下的使用升阻比，高亚声速时提高了5.9%，超声速时提高了10.3%，高超声速时提高了0.7%，解决了低速飞行时高升力与高速飞行时高升阻比的需求矛盾，并获得了一种满足宽速域总体设计要求的空天飞行器气动布局。研究成果具有一定工程指导意义。

Abstract

Aerospace vehicles have a wide velocity range that spans subsonic to hypersonic speeds. In such a wide speed range

their aerodynamic characteristics vary so significantly that traditional airfoils are improbable to satisfy the aerodynamic requirements for low- and high-speed flights at the same time. This paper proposes the requirements of airfoils and wings for aerospace vehicles

with especial attention being paid on the high lift at low speeds

high lift-to-drag ratio at high speeds

lift and gravity matching design

as well as structure and thermal protection design. In addition

an integrated design of airfoil and wing plane shape is carried out by numerical simulations based on a wide-speed-range airfoil. A new wing with spanwise-varying airfoils is obtained. Compared with the original wing

the lift efficiency of this new wing at low speed is increased by 36.3%. The lift-to-drag ratios at the lift-weight-balance point is increased by 33.4% and 12.9% respectively for supersonic and hypersonic flights. Since the new wing has good aerodynamic characteristics in the whole velocity range

it is further applied to a typical aerospace vehicle by an integrated optimization. The lift-to-drag ratio at the lift-weight-balance point is further improved by 5% at high subsonic speed

10.3% at supersonic speed

and 0.7% at hypersonic speed. The contradiction between high lift at low speed and high lift-to-drag ratio at high speed is alleviated. An aerospace vehicle layout that meets the overall design requirements for wide-speed-range flight is obtained. The results have certain engineering guiding significance.

关键词

Keywords

references

KUCZERA H, SACHER P W. Reusable space transportation systems[M]. WEI Y Y, ZHANG H W, WANG C Q, trans. Beijing: National Defense Industry Press, 2015.

WALDMAN B, HARSHA P. NASP: focus on techology[C]//4th International Aerospace Planes Conference, Orlando, FL, 1992. AIAA-92-5001.

HOEGENAUER E, KOELLE D. Saenger-the German aerospace vehicle program[C]// National Aerospace Plane Conference, Dayton, OH, USA. Reston, Virigina: AIAA, 1989. doi: 10.2514/6.1989-5007

BURNS B R A. HOTOL, an economic space transport for Europe[J]. Interdisciplinary Science Reviews, 1988, 13(2): 171-179. DOI:10.1179/isr.1988.13.2.171

LONGSTAFF R, BOND A. The SKYLON project[C]//17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, California. Reston, Virigina: AIAA, 2011. AIAA 2011-2244. doi: 10.2514/6.2011-2244

HUANG Z C. Sabre: new power for space shuttles[J]. Space International, 2015(7): 11-12. (in Chinese)

LING W H, HOU J L, WEI B X, et al. Technical challenge and potential solution for aerospace combined cycle engine[J]. Journal of Propulsion Technology, 2018, 39(10): 2171-2176. (in Chinese)

ZUO G, AI B C. Aerodynamic design of advanced space transportation system: Review[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(2): 624077. (in Chinese)

YUE T, WANG L X, AI J Q. Key technologies in morphing aircraft design[J]. Flight Dynamics, 2009, 27(5): 6-10. (in Chinese)

SUN Y, CHANG M, BAI J Q. Review of morphing wing aircraft[J]. Unmanned Systems Technology, 2021, 4(3): 65-77. (in Chinese)

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)

CAO C Q, CAI J S, DUAN Y H. Aerodynamic design optimization of supersonic airfoils[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(12): 3774-3784. (in Chinese)

SUN X C, HAN Z H, LIU F, et al. Design and analysis of hypersonic vehicle airfoil/wing at wide-range Mach numbers[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(6): 121737. (in Chinese)

YE Y D, ZHANG H X, JIANG Q X, et al. Some key problems in the study of aerodynamic characteristics of near-space hypersonic vehicles[J]. Chinese Journal of Theoretical and Applied Mechanics, 2018, 50(6): 1292-1310. (in Chinese)

HIRSCHEL E H, WEILAND C. Selected aerothermodynamic design problems of hypersonic flight vehicles[M]. TANG Z G, et al., trans. Beijing: National Defense Industry Press, 2013(in Chinese).

WANG L N. Research on aerodynamic problem and technology of aerospace vehicles[J]. Tactical Missile Technology, 2018(4): 32-37. (in Chinese)

LUO J L, KANG H L, CAO X L, et al. Aerodynamics of airbreathing hypersonic vehicles[M]. Beijing: Science Press, 2021.

吴子牛, 王兵, 周睿, 等. 空气动力学-下册[M]. 北京: 清华大学出版社, 2008.

ZHANG Y, HAN Z H, LIU F, et al. Multi-objective aerodynamic shape optimization of wide-Mach-number-range airfoil[J]. Physics of Gases, 2019, 4(4): 26-40. (in Chinese)

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. DOI:10.1016/j.ast.2019.105345

WEILAND CLAUS. Aerodynamic data of space vehicles[M]. TANG Z G, CHEN X L, trans. Beijing: Nationl Defense Industry Press, 2017.

SEDERBERG T W, PARRY S R. Free-form deformation of solid geometric models[C]// 13th annual conference on Computer graphics and interactive techniques - SIGGRAPH '86. New York: ACM Press, 1986. doi: 10.1145/15922.15903

CHEN S, BAI J Q, SUN Z W, et al. Aerodynamic optimization design of airfoil using DFFD technique[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(3): 695-705. (in Chinese)

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Impact of key area optimization on the aerodynamic characteristics of a high-speed train in crosswind

Research on interpretability of airfoil design based on sparse Bayesian optimization

Optimization design on the wing of a general aviation airplane based on deep belief network and multi-objective particle swarm optimization algorithm

Numerical simulation and optimization design of fluctuation pressure environment of a rocket fairing

Rotor airfoil aerodynamic design and evaluation software HRADesign

Related Author

Wang Lei

Gao Hongrui

Wang Xinran

Liu Tanghong

Jiang Jiyun

LIU Xuejun

YU Jian

LIU Zijing

Related Institution

中南大学交通运输工程学院，轨道交通安全教育部重点实验室

中南大学轨道交通安全关键技术国际合作联合实验室

中南大学轨道交通列车安全保障技术国家地方联合工程研究中心

中车长春轨道客车股份有限公司

MIIT Key Laboratory of Pattern Analysis and Machine Intelligence, College of Computer Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing

AI问答

⁰