Computational Finite Element Analysis of Adaptive Gas Turbine Stator-Rotor Flow Interactions for Future Vertical Lift Propulsion-Reference-Cited by-同舟云学术

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Computational Finite Element Analysis of Adaptive Gas Turbine Stator-Rotor Flow Interactions for Future Vertical Lift Propulsion

Published:2019-08-16 Issue: Volume: Page:
ISSN:
Container-title:AIAA Propulsion and Energy 2019 Forum
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Author:

Kozak Nikita S.¹,Bravo Luis G.²,Murugan Muthuvel²,Ghoshal Anindya²,Khine Yu Yu³,Bazilevs Yuri⁴,Hsu Ming-Chen¹

Affiliation:

1. Iowa State University

2. Army Research Laboratory

3. CREATE Kestrel Team

4. Brown University

Publisher

American Institute of Aeronautics and Astronautics

Reference33 articles.

1. NASA Technology for Next Generation Vertical Lift Vehicles

2. Welch, G. E., Skoch, G. J., and Thurman, D. R. “Foundational Aero Research for Development of Efficient Power Turbines with 50% Variable-speed Capability,” Tech. Rep. February 2011, U.S. Army Research Laboratory, 2011.

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