高超声速气动力试验模拟参数选取准则

doi:10.7527/S1000-6893.2014.0186

Abstract

Abstract:

Validity issue on simulation criterion for hypersonic aerodynamic test has hindered the development of ability on aerodynamic performance prediction for hypersonic aircraft. Scaling method is applied in the field of experimental aerodynamics within continuous flow regime. Various parametric scales are selected due to dual scale of flow characteristics and different parameters are applied to scaling the equation. Based on the assessment of the order of magnitude for each parameter, the simulation parameter and its weight are obtained for typical flight conditions. Results indicate that the analytical method supports the existing criterion of selective simulation parameters and provides suggestions to improve the simulation criterion. What is more, this paper illustrates that selective simulation parameters vary significantly as flight environment changes, and the ranking of simulation parameters is given by various flight conditions. By applying theoretical method, it is verified that viscous interaction parameter is one of the most significant simulation factors for hypersonic aerodynamic test, which coincides with conclusions of scholars abroad.

Key words: simulation parameters, scaling method, aerodynamic test, hypersonic, viscous interaction, wind tunnel test

CLC Number:

V411.7

WANG Gang, YANG Yanguang, TANG Zhigong. Criterion of selective simulation parameters for hypersonic aerodynamic test[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(3): 789-796.

References

[1] Frank K L. Advanced hypersonic test facilities[M]. Virginia: AIAA, 2002: 17-27.

[2] Tang Z Z. Hypersonic aerodynamic test[M]. Beijing: National Defense Industry Press, 2004: 45-53 (in Chinese). 唐志共. 高超声速气动力试验[M]. 北京: 国防工业出版社, 2004: 45-53.

[3] Kenneth W W, Mary F S. A comparison of hypersonic vehicle flight and prediction results, NASA/TM-104313[R]. Hampton.: NASA Langleg Resarch Center, 1995.

[4] Dinesh K P, Periklis E P, Carol B D, et al. Shuttle orbiter contingency abort aerodynamics: real gas effects and high angles of attack[C]//41st Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2003.

[5] Lin J Q. Deterministic problems applied to mathematics in natural science[M]. Beijing: Science Press, 2010: 238-256 (in Chinese). 林家翘. 自然科学中确定性问题的应用数学[M]. 北京: 科学出版社, 2010: 238-256.

[6] Tan Q M. Dimensional analysis[M]. Hefei: University of Science and Technology of China Press, 2007: 152-167 (in Chinese). 谈庆明. 量纲分析[M]. 合肥: 中国科学技术大学出版社, 2007: 152-167.

[7] Wu W Y. Fluid mechanics[M]. Beijing: Peking University Press, 2006: 171-179 (in Chinese). 吴望一. 流体力学[M]. 北京: 北京大学出版社, 2006: 171-179.

[8] White F M. Viscous fluid flow[M]. 2nd ed. New York: MaGraw-Hill Inc. Press, 1991: 233-253.

[9] Chen M Z. Fundamentals of viscous fluid dynamics[M]. Beijing: Higher Education Press, 2002: 24-27 (in Chinese). 陈懋章. 黏性流体动力学基础[M]. 北京: 高等教育出版社, 2002: 24-27.

[10] Anderson J D. Hypersonic and high temperature gas dynamics[M]. 2nd ed. Washington, D.C.: AIAA, 2006: 266-271.

[11] Bowcutt K G. Hypersonic vehicle systems integration:vehicle aerothermodynamic analysis and thermal management design[R]. Washington, D.C.: National Institute of Aerospace, 2007.

[12] Maus J R, Griffith B J, Szema K Y. Hypersonic Mach number and real gas effects on space shuttle orbiter aerodynamics[C]//21st Aerospace Sciences Meeting. Reston: AIAA, 1983.

[13] White A W, Arrington J P, McCandless R S. Performance aerodynamics of aero-assisted orbital transfer vehicles[C]//AIAA 22nd Aerospace Sciences Meeting. Reston: AIAA, 1984.

[14] Maus J R, Griffith B J, Tolbert D G. Understanding space shuttle flight data by use of wind tunneland CFD results[C]//AIAA 2nd Flight Testing Conference. Reston: AIAA, 1983.

[15] Plyashechnik V I. Investigation of the influence of parameter on the aerodynamic characteristics of a body of revolution with the contour generatrix break at hypersonic velocities, SPC94-4009[R]. Moscow: Central Aerodynamics Institute, 1998.

Criterion of selective simulation parameters for hypersonic aerodynamic test

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Pengpeng SUN, Ping’an LIU, Feng FAN, Wei ZENG. Aerodynamic interaction characteristics of coaxial rigid rotor⁃fuselage in hover condition [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529284-529284.
[2]	Chang WANG, Long HE, Dongxia XU, Min TANG, Shuai MA, Ximing WU. Flow control drag reduction of hub on coaxial rigid rotor aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529084-529084.
[3]	Weiguo ZHANG, Min TANG, Jie WU, Xianmin PENG, Guichuan ZHANG, Bowen NIE, Liangquan WANG, Chaoqun LI. Overview of wind tunnel test research on tiltrotor aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 530114-530114.
[4]	Bowen NIE, Liangquan WANG, Zhiyin HUANG, Long HE, Shipeng YANG, Hongtao YAN, Guichuan ZHANG. Flight dynamics modeling and control scheme design of compound high-speed unmanned helicopters [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529848-529848.
[5]	Jiancheng ZHENG, Zhiguo QU, Xiansi TAN, Zhihuai LI, Gang ZHU, Lujun LI, Wei LIU. Resource management for hypersonic target detection by radar network based on responsibility area partitioning [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(8): 329022-329022.
[6]	Qichang CHEN, Zhiwei SHI, Weiyuan ZHANG, Linglong YAO, Shengxiang TONG. Aerodynamic layout and control strategy design and flight verification of a wing⁃foldable variant VTOL aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 629583-629583.
[7]	Liu LIU, Xianhong XIANG, Yufei ZHANG, Haixin CHEN, Chuang WEI, Jian ZHU, Pu YANG. A high lift-to-drag ratio unconventional blended-wing-body aerodynamic configuration with swallow tail [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 629630-629630.
[8]	Jinzhao DAI, Haixin CHEN. Optimization design method of three⁃dimensional wave cancellation biplane derived by shock⁃wave morphology [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 628942-628942.
[9]	Xiaoyong LIU, Mingfu WANG, Jianwen LIU, Xin REN, Xuan ZHANG. Review and prospect of research on scramjet [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(5): 529878-529878.
[10]	Bo YANG, He YU, Zichen FAN. Micro-energy analysis method for time-varying error of aero-optical effects [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(4): 128703-128703.
[11]	Haixing LI, Feng ZHOU, Wei YAN, Feng BAI, Keliang ZHAO. Effects of roughness ice on aerodynamic performance of civil aircraft horizontal tail [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128657-128657.
[12]	Xueliang LI, Chuangchuang LI, Wei SU, Jie WU. Experiment of influence of distributed roughness elements on hypersonic boundary layer instability [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128627-128627.
[13]	Jiang LAI, Zhaolin FAN, Qian WANG, Siwei DONG, Fulin TONG, Xianxu YUAN. Direct numerical simulation of hypersonic cone-flare model at angle of attack [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128610-128610.
[14]	Youde XIONG, Chuangchuang LI, Zhenhui ZHANG, Jie WU. Measurement of freestream disturbance in hypersonic wind tunnel with hot-wire anemometer [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(10): 129042-129042.
[15]	Yu LIU, Mengjie QIN, Qiang WANG, Xian YI. Scaling law for salty sea spray icing wind tunnel test [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729297-729297.