Effects of airfoil-probe tubes on the flow field of a compressor cascade

Author:

Ma Hongwei,Jin Chao,Zhao Lianpeng,Ma Rong

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference15 articles.

1. Dudzinski T. J. Effect of inlet geometry on flow-angle characteristics of miniature total pressure tubes. NASATN-D-6404

2. Biela C., Muller M. W., Schiffer, et al. Unsteady pressure measurement in a single stage axial transonic compressor near the stability limit. ASME GT2008-50245

3. Lehmann K. and Happel H. W. Comparison of transonic flow calculations with experimental data. London: ASME Gas Turbine Conference, 1982

4. Lecheler S., Schnell R. and Stubert B. Experimental and numerical investigation of the flow in a 5-stage transonic compressor rig. ASME 2001-GT-0344

5. Coldrjck S, Lvey P C, Wells R G. The influenc of compressor aerodynamics on pressure probe part1: in rig clibrations. ASME 2004-GT-53240, 2004

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