January 01, 1996 article Improved Blade Profile Loss and Deviation Angle Models for Advanced Transonic Compressor Bladings: Part II—A Model for Supersonic Flow Journal of Turbomachinery DOI: 10.1115/1.2836610 OpenAlex Authors 0 Author list not loaded yet. Cited by 1 stored of 43 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 A region-segmentation combinational loss model based on data-driven machine learning for a boundary layer ingestion fan 2023 Aerospace Science and Technology article Engineering Turbomachinery Performance and Optimization 9 citations 1 result References 0