Performance of a high-work low aspect ratio turbine tested with a realistic inlet radial temperature profile-Reference-Cited by-同舟云学术

Performance of a high-work low aspect ratio turbine tested with a realistic inlet radial temperature profile

Published:1984-06-11 Issue: Volume: Page:
ISSN:
Container-title:20th Joint Propulsion Conference
language:
Short-container-title:

Author:

STABE R.¹,WHITNEY W.¹,MOFFITT T.¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1161

Reference14 articles.

1. Katsanis, T. and McNally, W. D. "Revised FORTRAN Program for Calculating Velocities and Streamlineson the Hub-Shroud Midchannel Stream Surface of an Axial- Radial- or Mixed-Flow Turbomachine or Annular Duct - I User's Manual, NASA-TN-0-0430, 1977.

2. Whitney, W. J., Stabe, R. G., and Moffitt, T. P. "Description of the Warm Core Turbine Facility Recently Installed at NASA Lewis Research Center, NASA-TM-81562, 1980.

Cited by 29 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. Optimization of thermal management system architecture in hydrogen engine employing improved genetic algorithm;Energy;2024-06

2. Part-load thermal efficiency enhancement in gas turbine combined cycles by exhaust gas recirculation;Applied Thermal Engineering;2024-05

3. Unsteady Flows and Component Interaction in Turbomachinery;International Journal of Turbomachinery, Propulsion and Power;2024-04-05

4. Fully Coupled Body Force–Engine Performance Methodology for Boundary Layer Ingestion;Journal of Propulsion and Power;2021-03

5. Statistical and Computational Evaluation of Axial Loss Correlations Applied to Centrifugal Turbines;AIAA Propulsion and Energy 2020 Forum;2020-08-17