Wave engine topping cycle assessment-Reference-Cited by-同舟云学术

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Wave engine topping cycle assessment

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Welch G.¹,Welch G.¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-707

Reference19 articles.

1. 'Pearson, R. D. "A Gas Wave-Turbine Engine which Developed 35 H.P. and Performed over a 6:1 Speed Range," eds.,Shreeve, R.P.andMathur,A., Proc.1985 ONR/NAVAIR Wave Rotor Research and Technology Workshop, Report NPS-67-85-008, Naval Postgraduate School, Monterey, CA, May, 1985, pp.125-170.

2. 2Pearson, R. D. "Performance Predictions for Gas Wave Turbines including Practical Cycles with Wide Speed Range," ibid., pp.329-378.

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1. Nuclear Wave Rotor Bi-Modal Cycle for In-Space Propulsion;AIAA SCITECH 2024 Forum;2024-01-04

2. Validation of a Numerical Quasi-One-Dimensional Model for Wave Rotor Turbines With Curved Channels;Journal of Engineering for Gas Turbines and Power;2020-01-17

3. A Review of Wave Rotor Technology and Its Applications;Journal of Engineering for Gas Turbines and Power;2006

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