SUPERSONIC AND TRANSONIC AERODYNAMIC CHARACTERISTICS OF SB301 TWO-DIMENSIONAL CASCADE WIND TUNNEL

Jiang Zhengli; Ma Jinxian

Volume 2 Issue 2

Apr. 1987

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Article Navigation > Journal of Aerospace Power > 1987 > 2(2): 162-164,189-190

Jiang Zhengli, Ma Jinxian. SUPERSONIC AND TRANSONIC AERODYNAMIC CHARACTERISTICS OF SB301 TWO-DIMENSIONAL CASCADE WIND TUNNEL[J]. Journal of Aerospace Power, 1987, 2(2): 162-164,189-190.

Citation:

Jiang Zhengli, Ma Jinxian. SUPERSONIC AND TRANSONIC AERODYNAMIC CHARACTERISTICS OF SB301 TWO-DIMENSIONAL CASCADE WIND TUNNEL[J]. Journal of Aerospace Power, 1987, 2(2): 162-164,189-190.

Jiang Zhengli, Ma Jinxian. SUPERSONIC AND TRANSONIC AERODYNAMIC CHARACTERISTICS OF SB301 TWO-DIMENSIONAL CASCADE WIND TUNNEL[J]. Journal of Aerospace Power, 1987, 2(2): 162-164,189-190.

Citation:

Jiang Zhengli, Ma Jinxian. SUPERSONIC AND TRANSONIC AERODYNAMIC CHARACTERISTICS OF SB301 TWO-DIMENSIONAL CASCADE WIND TUNNEL[J]. Journal of Aerospace Power, 1987, 2(2): 162-164,189-190.

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SUPERSONIC AND TRANSONIC AERODYNAMIC CHARACTERISTICS OF SB301 TWO-DIMENSIONAL CASCADE WIND TUNNEL

Gas Turbine Establishment

Received Date: 1986-08-01
Publish Date: 1987-04-28

Abstract

Abstract

SB301 wind tunnel was designed to test two-dimensional cascades of compres- sor in subsonic,transonic and supersonic flow. The wind tunnel has been equipped with advanced instrumentation and enables to accomplish a wide range of experimentation. It is first successful one for testing the two-dimensional cascades of compressor in transonic and supersonic flow in China by now. It provides a new test rig for research and development of aeroengines with high performances.