Total unsteadiness analysis for an axial-flow compressor rotor
Author:
Affiliation:
1. Virginia Polytechnic Inst. and State Univ., Blacksburg
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-967
Reference8 articles.
1. Three-Dimensional Flow and Mixing in an Axial Flow Compressor With Different Rotor Tip Clearances
2. Isomura, K., and Giles, M.B., 1995, "A Numerical Simulation of the Unsteadiness in a Transonic Steady-State Blade to Blade Flow in NASA Rotor 67," Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Elsevier Science B.V.
3. Moore, J.G., Liu, B., and Moore, J., 1997, " New Twists on the Deverson Axial-Flow Compressor Rotor,"ASMEPaper 97-GT-100.
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Total Unsteadiness Downstream of an Axial Flow Fan With Variable Pitch Blades;Journal of Fluids Engineering;2001-09-10
2. Unsteady Flow Pattern Characteristics Downstream of a Forward-Curved Blades Centrifugal Fan;Journal of Fluids Engineering;2000-12-11
3. Turbulence energy and spectra downstream of an axial compressor rotor;29th AIAA, Fluid Dynamics Conference;1998-06-15
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