Published August 1, 2018 | Version v1
Journal article

A Computational Fluid Dynamic Study for Temperature Uniformity at a Wind Tunnel Outlet with Effects of Heat Transfer along Tunnel Walls

  • 1. State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, P R China (China)
  • 2. Advanced Analysis Group, Advisian Singapore (WorleyParsons Group), #13-03 TripleOne Somerset, 111 Somerset Road, Singapore, 238164 (Singapore)

Description

A Computational Fluid Dynamics (CFD) Modelling was carried out to investigate temperature uniformity at a wind tunnel outlet region to benefit its design and construction. Low temperate (110K) nitrogen entered the wind tunnel at inlet, passed through two turning area with 18 turning vanes and went into expansion session, stable session and congestion session, finally towards outlet discharge nozzle session. The model considered static nitrogen isolation layer in physical model and three more isolation layer outside the tunnel as well as possible heat transfer from ambient environment. Two case scenario for supersonic and subsonic at outlet (Mach Number 0.9 and 1.3) were conducted with a uniform temperature imposed at inlet, as well a 3rd case scenario (Mach Number 0.9) with a non-uniform temperature distribution at inlet. Existence of porous zone (to model honeycomb session) and porous interfaces (to model damping interfaces) at the stable session were also included. Contours of temperature and velocity on representative cross sections were presented, and effects of Mach number, total pressure and initial temperature distribution at inlet on temperature uniformity at outlet were discussed. Based on the numerical results, improvement of tunnel geometry for better flow uniformity at outlet regions were also suggested. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1757-899X/408/1/012003

Additional details

Publishing Information

Journal Title
IOP Conference Series. Materials Science and Engineering (Online)
Journal Volume
408
Journal Issue
1
Journal Page Range
[7 p.]
ISSN
1757-899X

Conference

Title
2. International Conference on Advanced Technologies in Design, Mechanical and Aeronautical Engineering
Acronym
ATDMAE 2018
Dates
1-3 Jul 2018
Place
Dalian (China)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
52094547
Subject category
S42: ENGINEERING; S71: CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS;
Resource subtype / Literary indicator
Conference
Descriptors DEI
COMPUTERIZED SIMULATION; CROSS SECTIONS; DAMPING; FLUID MECHANICS; FLUIDS; GEOMETRY; HEAT TRANSFER; MACH NUMBER; NITROGEN; POROUS MATERIALS; TEMPERATURE DISTRIBUTION; TUNNELS; WIND TUNNELS
Descriptors DEC
DIMENSIONLESS NUMBERS; ELEMENTS; ENERGY TRANSFER; EQUIPMENT; MATERIALS; MATHEMATICS; MECHANICS; NONMETALS; SIMULATION; UNDERGROUND FACILITIES; VELOCITY