Investigation of longitudinal airflow characteristics in an aircraft cabin based on angle of attack

被引:1
作者
Xing, Zihan [1 ]
Zhang, Yongzhi [1 ]
Wang, Ping [1 ]
Zhang, Jiaxing [1 ]
机构
[1] Donghua Univ, Coll Environm Sci & Engn, Room 221,Integrated Lab Bldg,2999 North Renmin Rd, Shanghai 201620, Peoples R China
基金
中国国家自然科学基金;
关键词
Aircraft cabin; angle of attack; longitudinal airflow; scaled model; vortex structure; MIXED CONVECTION; TURBULENCE MODELS;
D O I
10.1177/1420326X241237930
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
As an important means of transportation, an aircraft's environmental control system plays an important role in ensuring the health and thermal comfort of the cabin environment. To guarantee sufficient lift during flight, the aircraft cabin needs to have a certain angle of attack with the horizontal direction. In this study, the flow field, temperature field and vortex structure characteristics of the cabin were analysed using a scaled 28-row cabin model and computational fluid dynamics (CFD) under different angles of attack (15 degrees and 8 degrees) conditions. The results show that the velocity and temperature in the local area in the longitudinal section were increased when the angle of attack was increased. Compared with the horizontal state (angle of attack 0 degrees), the longitudinal airflow under the condition of a larger angle of attack was enhanced. The overall trend of forward airflow is presented in this paper. The longitudinal airflow would strengthen the separation of the large vortex at the top of the cabin. The vortex structure shows high instability in different times and spaces.
引用
收藏
页码:1280 / 1298
页数:19
相关论文
共 50 条
[41]   Modeling and simulation of aircraft attitude angle based on air-path [J].
Yuan X.-J. ;
Zhao X.-J. ;
Li J.-L. .
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics, 2016, 38 (04) :889-894
[42]   Calculation of Warhead Reentry Angle of Attack based on Flight Test Data [J].
Fan, Jinhua ;
Song, Jianying ;
Peng, Jie .
PROCEEDINGS OF THE 28TH CHINESE CONTROL AND DECISION CONFERENCE (2016 CCDC), 2016, :5121-5124
[43]   An angle of attack-based derailment criterion for wheel flange climbing [J].
Guan, Qinghua ;
Zeng, Jing ;
Jin, Xuesong .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART F-JOURNAL OF RAIL AND RAPID TRANSIT, 2014, 228 (07) :719-729
[44]   Wind turbine airfoil optimal design based on a multipoint angle of attack [J].
Wang Q. ;
Wang J. ;
Chen J. ;
Yu X. ;
Sun J. .
Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University, 2016, 37 (11) :1580-1585
[45]   Angle of Attack Control of a Blended Wing Body Aircraft Using State Feedback L1 Adaptive Controller [J].
Zheng, FuLei ;
Xu, Jun .
2013 CHINESE AUTOMATION CONGRESS (CAC), 2013, :738-743
[46]   Analytical Synthesis of Stabilization Laws of Coupled Motions of an Aircraft in the Pitch–Yaw Channels in the Absence of Information about the Angle of Attack [J].
Zubov N.E. ;
Ryabchenko V.N. ;
Lapin A.V. .
Russian Aeronautics, 2022, 65 (1) :99-110
[47]   Building a Camera-based Smart Sensing System for Digitalized On-demand Aircraft Cabin Readiness Verification [J].
Unzueta, Luis ;
Garcia, Sandra ;
Garcia, Jorge ;
Corbin, Valentin ;
Aranjuelo, Nerea ;
Elordi, Unai ;
Otaegui, Oihana ;
Danielli, Maxime .
PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON ROBOTICS, COMPUTER VISION AND INTELLIGENT SYSTEMS (ROBOVIS), 2020, :98-105
[48]   Knowledge-based model generation for aircraft cabin noise prediction from pre-design data [J].
Hesse, Christian ;
Allebrodt, Pia ;
Teschner, Mark ;
Biedermann, Jörn .
CEAS Aeronautical Journal, 2024, 15 (04) :1127-1136
[49]   Angle of Attack Characteristics of Full-Active and Semi-Active Flapping Foil Propulsors [J].
Mei, Lei ;
Yan, Wenhui ;
Zhou, Junwei ;
Tang, Yongqi ;
Shi, Weichao .
WATER, 2024, 16 (20)
[50]   INVESTIGATION OF FLOW CHARACTERISTICS AND VORTEX FORMATIONS OF LAMBDA WING AT HIGH ANGLES OF ATTACK [J].
Yavuz, M. Murat .
JOURNAL OF THERMAL ENGINEERING, 2020, 6 (06) :282-297