Description
Book Synopsis
Proceedings of the NATO Advanced Study Institute, Montechoro, Algarve, Portugal, April 16-27, 1990
Table of Contents
1. Modem Diagnostic Techniques for Combusting Flows: An Overview.- 2. Fundamental Aspects of Gaseous Combustion.- 3. Three-Dimensional Structure of Strongly Forced Jet Diffusion Flames: Flow Visualization Studies.- 4. Probe Measurements of Scalar Properties in Reacting Flows.- 5. Planar Fluorescence Imaging: Basic Concepts for Scalar and Velocity Measurements.- 6. Degenerate Four Wave Mixing and Coherent Anti-Stokes Raman Scattering: Applications in Combustion Diagnostics — Species Imaging and Improved Temperature Measurements.- 7. Probe and Optical Techniques for Simultaneous Scalar-Velocity Measurements.- 8. Optically-Based Measurement Techniques for Dispersed Two Phase Flows.- 9. Quasi-Elastic Light Scattering and Applications to Optical Sizing.- 10. Optical Measurements of Gas Phase Vector and Scalar Properties in Reacting and Non- reacting Polydispersed Sprays.- 11. Quantitative Flow Measurement System Using the PIV Technique.- 12. A New Technique for 3D Instantaneous Velocity Measurements, with Special Emphasis on Combustion.- 13. Aircraft Turbine Engine Combustors — Development Status/Challenges.- 14. Review of Recent Measurements in Gas Turbine Combustors.- 15. Coherent Laser Diagnostics for Temperature/Species Measurements in Advanced Engines.- 16. Experimental Characterization of Diesel Engines.- 17. High Speed Optical Diagnostics of Combustion Diesel Fuel Sprays.- 18. Mixture Formation in a Spray Observed by Spontaneous Raman Spectroscopy.- 19. Techniques for Detecting Flame Arrival in Premixed-Charge Spark Ignition Engines.- 20. CARS Spectroscopy for Temperature and Concentration Measurements in a Spark Ignition Engine.- 21. Application of Fiber LDV for Flow Measurements in a Two-Stroke Engine.- 22. The Measurement and Interpretation of the Starch Dust-Air Explosion Parameters in a Closed Spherical Vessel.- 23. Raman Scattering on Evaporating Single Microparticles.- 24. Determination of Aircraft Pressure Altitude and Ambient Temperature Using Fluorescence and Rayleigh Scattered Radiation from a Continuum Source.
