Interferometric Study of Unsteady Passing Shock Flow in a Turbine Cascade-Reference-Cited by-同舟云学术

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Interferometric Study of Unsteady Passing Shock Flow in a Turbine Cascade

Published:1999-07 Issue:4 Volume:15 Page:489-496
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Wesner A.¹,Schetz J. A.²,Grabowski H.²

Affiliation:

1. Johns Hopkins University, Applied Physics Laboratory, Laurel, Maryland 27023

2. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061-0203

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.5463

Reference18 articles.

1. 2Janakiraman, S. V. “Fluid Flow and Heat Transfer in Transonic Turbine Cascades,” M.S. Thesis, Mechanical Engineering Dept., Virginia Polytechnic Inst.and State Univ., Blacksburg, VA,May 1993.

2. Simulation of the Effects of Shock Wave Passing on a Turbine Rotor Blade

3. Vane-blade interaction in a transonic turbine. I - Aerodynamics

4. 5Kiss, T. “Experimental and Numerical Investigation of Transonic Turbine Cascade Flow,” Ph.D. Dissertation, Mechanical Engineering Dept., Virginia Polytechnic Inst.and State Univ., Blacksburg, VA,Dec. 1992.

Cited by 1 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. Unsteady Heat Transfer Measurements from Transonic Turbine Blades at Engine Representative Conditions in a Transient Facility;Journal of Engineering for Gas Turbines and Power;2008

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