Open Access
ARTICLE
HEAT TRANSFER BASED NUMERICAL INVESTIGATION OF AIRCRAFT CABIN ENVIRONMENT FROM VARIOUS INLET CONDITIONS
Zhuohuan Hua,*, Lulu Wanga, Hui Wangb, Mo Yanga
a
School of Energy and Power Engineering, University of Shanghai for Science and Technology, Shanghai, 200093, China
b
National Computer Network and Information Safety Administration Center Shanghai Network Access Point, Shanghai, 201315, China
* Corresponding Author: Email:
Frontiers in Heat and Mass Transfer 2015, 6, 1-8. https://doi.org/10.5098/hmt.6.16
Abstract
A numerical investigation was conducted to study the heat transfer in an aircraft cabin and the effects of air distribution under different angle and
inlet velocity conditions. The Reynolds-averaged Navier–Stokes equations and the low Reynolds number turbulence model were used to simulate the
airflow in the cabin. Mathematical statistics was used to process the relevant data, and statistical results revealed that different inlet angles and
velocities significantly affect air temperature and flow field. The study also determined a set of optimum matching inlet vane angles and inlet
velocities that result in an environment which meets standard requirements and is energy saving. Additional studies were also conducted on the
thermal comfort in cabin environments under optimal conditions. The conclusions of this thesis are scientific and feasible, and they can be used to
improve the comfortableness of cabin environments.
Keywords
Cite This Article
Hu, Z., Wang, L., Wang, H., Yang, M. (2015). HEAT TRANSFER BASED NUMERICAL INVESTIGATION OF AIRCRAFT CABIN ENVIRONMENT FROM VARIOUS INLET CONDITIONS.
Frontiers in Heat and Mass Transfer, 6(1), 1–8. https://doi.org/10.5098/hmt.6.16