简体中文 English  

 

Home   About us   Product   Service & Support   Download Center    Message Board   Contact us

user name:
password  :
 
·forget password Please click here!
 
AVIC Aerodynamics Research Institute
Harbin

Address: No.2, Yiman Street, Nangang District, Harbin, Heilongjiang Province, China  No. 88 PO-Box, Harbin, China
Post Code: 150001
Tel : 0086-451-82521573
Fax: 0086-451-82511688
Website: www.avicari.com.cn
E-mail: avicari@avicari.com.cn
Shenyang
Address: No.1, YangShan Street, Huanggu District, Shenyang, Liaoning Province, China No. 701 PO-Box, Shenyang, China
Post Code: 110034
Tel : 0086-24-86512103
Fax: 0086-24-86520827
E-mail: avicari@avicari.com.cn
 
 

  AVIC Aerodynamics Research Institute (hereinafter referred to as “AVIC ARI ") is under the governance of Aviation Industry Corporation of China (AVIC). It was established by merging former Harbin Aerodynamics Research Institute (founded in 1955) with Shenyang Aerodynamics Research Institute (founded in 1958) in 2000. At present, the permanent staff of AVIC ARI totaled over 800 employees in which more than 600 of them are technicians...

Wind tunnel for aviation
FL-6 TPS(turbine power simulator)calibration tank
FL-5 Low Speed Wind Tunnel
FL-3 High Speed Wind Tunnel
FL-2 High Speed Wind Tunnel
FL-1 Trisonic High Speed Wind Tunnel
FL-9 Pressurized low speed wind tunnel
FL-8 low speed wind tunnel
 
·Aircraft Static Aerodynamic
  Performances Test
·Aircraft Dynamic Aerodynamic
  Performances Test
·Engine Simulation Test
·Aircraft Maneuver Characteristic
  Test
·Inlet Performances Test
·High/Variable Reynolds Number
  Test
·External Store Jettison and
  Separation Test
·Multi-balance Components and
  Hinge Moment Test
·OPS and PSP
·Multi-Sheet Light Flow
  Visualization and Image
  Manipulation Technique
·PIV Technique
·CFD Software Design and
  Development
·CFD engineering applications
·The Multi-Subject and Multi-
  Objective Optimization Design
·Fixed-Wing Aircraft Configuration
  Research
·Fan-wing Aircraft
·Study on Complex Flow
  Mechanism (free-rolling and
  free-yawing tests)
·Synthetic Jet Flow
·Plasma Drag Decrease
 
   
 

Webpage Copyright(c)2009-2011 www.avicari.com.cn  Powered by: www.ce.net.cn 黑ICP备06002346号