Low Reynolds number loss reduction on turbine blades with dimples and V-grooves-Reference-Cited by-同舟云学术

Low Reynolds number loss reduction on turbine blades with dimples and V-grooves

Published:2000-01-10 Issue: Volume: Page:
ISSN:
Container-title:38th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Lake James¹,King Paul²,Rivir Richard¹

Affiliation:

1. USAF, Research Lab., Edwards AFB, CA

2. USAF, Inst. of Technology, Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-738

Reference12 articles.

1. [I] Lake, J.P "Flow Separation Prevention on aTurbine Blade at Low Reynolds Number." PhD dissertation,Air Force Institute of Technology, June 1999.AFIT No. AFITDS-ENY-99-0 1.

2. Reduction of separation losses on a turbine blade with low Reynolds numbers

3. Boundary Layer Development in Axial Compressors and Turbines: Part 1 of 4 — Composite Picture

4. Boundary Layer Development in Axial Compressors and Turbines: Part 3 of 4 — LP Turbines

Cited by 44 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. Effects of Heat Transfer on Laminar-to-Turbulent Transition over a Compressor Blade Operating at Low Reynolds Number;Journal of Thermal Science;2024-07-11

2. Enhancing Flow Separation Control Using Hybrid Passive and Active Actuators in a Matrix Configuration;Aerospace;2024-05-23

3. Control of separation flows of turbine-blade-tip turbines by splitter blades;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2024-05-08

4. Study of the influence of multiple factors on the boundary layer of a high-lift LPT with the RBF-GA method;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-11-24

5. Numerical Studies on the Effect of Leading Edge Tubercles on a Low-Pressure Turbine Cascade;Energies;2023-05-30