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�������պ����ѧѧ�� 2010, Vol. 36 Issue (12) :1436-1439,1452    DOI:
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���農, ������, ��ѩ��*
�������պ����ѧ ���տ�ѧ�빤��ѧԺ, ���� 100191
Airflow thermal simulation and comfort evaluation of commercial airliner
Wang Lijing, Wang Zhaoxin, He Xueli*
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

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Abstract�� Air velocity field and temperature field of cockpit will affect the pilots- thermal comfort and performance directly, which are important parts need to be considered in the design of cockpit structure and environmental control system. After full-size three-dimensional model of B737-800 cockpit being established, a commercial computational fluid dynamics(CFD) software Fluent was used to calculate the flow field and temperature field of cockpit in high-altitude night work. Then the average temperature evaluation and the predicted mean vote(PMV)on the thermal sensation scale were used to evaluate cockpit temperature environment. A questionnaire was given to the pilot to obtain cockpit air flow and temperature comfort subjective evaluation. The results of simulation and subjective evaluation both indicate the B737-800 cockpit is a comfortable environment at night at high altitude. Besides, the trunk and legs feel a little uncomfortable as a result of slight coolness. The agreement of simulation results and evaluation results validates the accuracy of the cockpit airflow thermal simulation.
Keywords�� numerical simulation   velocity field   temperature field   evaluation     
Received 2010-07-31;


About author: ���農(1965-),Ů,ɽ��۩����,������,wanglijing@buaa.edu.cn.
���農, ������, ��ѩ��.���Ϳͻ���ʻ�������ȷ��漰����������[J]  �������պ����ѧѧ��, 2010,V36(12): 1436-1439,1452
Wang Lijing, Wang Zhaoxin, He Xueli.Airflow thermal simulation and comfort evaluation of commercial airliner[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2010,V36(12): 1436-1439,1452
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