October 20, 2010 article Compressor Leading Edge Spikes: A New Performance Criterion Journal of Turbomachinery DOI: 10.1115/1.4000567 OpenAlex Authors 0 Author list not loaded yet. Cited by 2 stored of 87 Search Sort Most cited Newest Oldest Patent citations Title Any typearticle review book-chapter conference-paper preprint dissertation book dataset other Any fieldAgricultural and Biological Sciences Arts and Humanities Biochemistry, Genetics and Molecular Biology Business, Management and Accounting Chemical Engineering Chemistry Computer Science Decision Sciences Dentistry Earth and Planetary Sciences Economics, Econometrics and Finance Energy Engineering Environmental Science Health Professions Immunology and Microbiology Materials Science Mathematics Medicine Neuroscience Nursing Pharmacology, Toxicology and Pharmaceutics Physics and Astronomy Psychology Social Sciences Veterinary Open access Manufacturing Considerations in the Aerodynamic Design Process of Turbomachinery Components 2025 Processes article Engineering Turbomachinery Performance and Optimization Open access 1 citations Performance Analysis of a Compressor Leading Edge without Pressure Spike at High Subsonic Speed 2020 International Journal of Gas Turbine Propulsion and Power Systems article Engineering Turbomachinery Performance and Optimization Open access 1 citations 2 results References 0