Modified Characteristic Method for Calculation of Supersonic S2 Flow Field in Compressor

Articles in the same Issue

1. CONTENTS
2. In-Flight Short Field Landing Investigations on a Combat Aircraft with Thrust Reverser
3. Distribution of Mean Concentration, Dropsize and Velocity, and Size-Velocity Correlations in the Spray of an Air-assist Nozzle
4. Combined Influence of Unsteady Free Stream Velocity and Free Stream Turbulence on Stagnation Point Heat Transfer
5. Experimental Research on Air Flow through Liner Holes
6. Measurement of Swirling Flow Field Using the Single-Slanted Hot-Wire Technique
7. Emissions from Enclosed Swirl Stabilised Premixed Flames
8. Conical Grid Plate Flame Stabilizers: Stability and Emissions for Liquid Fuels
9. Conical Grid Plate Flame Stabilizers for Combustor Primary Zones
10. A Preliminary Study of Annular Diffusers with Constant Diameter Outer Walls (Suitable for Turbine Exits)
11. An Experimental and Theoretical Investigation of an Uncentralized Squeeze-Film Damper Bearing and the Test Results on a Jet Engine
12. Effect of Air Pressure upon Spray Angle/Width Characteristics of Simplex Pressure Swirl Atomizers
13. A Two-Dimensional Finite Element Stress Analysis of Radial Impellers
14. Modified Characteristic Method for Calculation of Supersonic S2 Flow Field in Compressor
15. Fuel Effects on Gas Turbine Combustion
16. Transpiration Cooling: Contribution of Film Cooling to the Overall Cooling Effectiveness