Axial Bladeless Turbine Suitable for High Supersonic Flows-Reference-Cited by-同舟云学术

Axial Bladeless Turbine Suitable for High Supersonic Flows

Published:2016-07 Issue:4 Volume:32 Page:975-983
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Vinha Nuno¹,Paniagua Guillermo²,Sousa Jorge³,Saracoglu Bayindir H.³

Affiliation:

1. Universidad Politécnica de Madrid, 28040 Madrid, Spain

2. Purdue University, West Lafayette, Indiana 47907

3. von Karman Institute for Fluid Dynamics, 1640 Sint-Genesius-Rode, Belgium

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/10.2514/1.B35818

Reference12 articles.

1. Supersonic cascade flow

2. GoldmanL. J.ScullinV. J. “Analytical Investigation of Supersonic Turbomachinery Blading 1—Computer Program for Blading Design,” NASA TN-D-4421, 1968.

3. Aerodynamic Design and Verification of a Two-Stage Turbine With a Supersonic First Stage

4. The Supersonic Axial Inlet Component in a Compressor

5. Design and analysis of pioneering high supersonic axial turbines

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