发文地区与机构
近年国家 / 地区发文量统计
| 国家 / 地区 | 发文量 |
|---|---|
| USA | 110 |
| England | 93 |
| GERMANY (FED REP GER) | 68 |
| CHINA MAINLAND | 52 |
| Italy | 36 |
| France | 15 |
| Switzerland | 13 |
| NORTHERN IRELAND | 11 |
| Sweden | 11 |
| Australia | 10 |
近年机构发文量统计
| 机构 | 发文量 |
|---|---|
| ROLLS-ROYCE HOLDING GROUP | 40 |
| UNIVERSITY OF CAMBRIDGE | 29 |
| UNIVERSITY OF OXFORD | 28 |
| GENERAL ELECTRIC | 22 |
| PENNSYLVANIA COMMONWEALTH SYSTEM OF HIG... | 17 |
| IMPERIAL COLLEGE LONDON | 16 |
| RAYTHEON TECHNOLOGIES | 14 |
| UNIVERSITY OF FLORENCE | 13 |
| QUEENS UNIVERSITY BELFAST | 11 |
| SHANGHAI JIAO TONG UNIVERSITY | 11 |
文章引用情况
1
Validation of a Numerical Model for Predicting Stalled Flows in a Low-Speed Fan-Part II: Unsteady Analysis2
The Inner Workings of Axial Casing Grooves in a One and a Half Stage Axial Compressor With a Large Rotor Tip Gap: Changes in Stall Margin and Efficiency3
Effect of Internal Crossflow Velocity on Film Cooling Effectiveness-Part I: Axial Shaped Holes4
Heat Transfer Coefficient and Film Cooling Effectiveness on the Partial Cavity Tip of a Gas Turbine Blade5
Effect of Internal Crossflow Velocity on Film Cooling Effectiveness-Part II: Compound Angle Shaped Holes6
Transonic Compressor Blade Optimization Integrated With Circumferential Groove Casing Treatment7
Large Eddy Simulation and RANS Analysis of the End-Wall Flow in a Linear Low-Pressure-Turbine Cascade-Part II: Loss Generation8
Effects of Bio-Inspired Micro-Scale Surface Patterns on the Profile Losses in a Linear Cascade9
Evaluation of Compressor Blading With Blade End Slots and Full-Span Slots in a Highly Loaded Compressor Cascade10
Cooling Effectiveness for a Shaped Film Cooling Hole at a Range of Compound Angles