A Computer Program for the Specification of Axial Compressor Airfoils
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Defense Technical Information Center
Cited by 6 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. Investigations on Design Space for Highly Loaded Tandem Bladed Axial Flow Rotor- novel Stator for Low-speed Compressor Research Facility;Journal of Applied Fluid Mechanics;2024-10-01
2. Enhancing transonic compressor rotor efficiency by flow analysis-driven blade section modification;International Journal of Turbo & Jet-Engines;2024-07-30
3. A flexible method for geometric design of axial compressor blades;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-02-23
4. Computational Method in the Throughflow Simulation of Aeroengine Compressor;Proceedings of the International Conference on Aerospace System Science and Engineering 2020;2021
5. Effect of Leading Edge Stacking on the Aerodynamic Performance of a Multistage Axial Flow Compressor;Journal of Aerospace Sciences and Technologies;2020-02-01
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