180 results on '"Campbell D"'
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2. Investigation of Extinction and Turbulence Effects in Liquid-Fueled Jet Flames
3. Application of C-X band CH PLIF to Topological Studies of Turbulent Spray Flames
4. Application of C-X band CH PLIF to Topological Studies of Turbulent Spray Flames
5. Exploration of Two-Phase Flow Structures in Metal Nozzles with Various Configurations Using X-Ray Fluorescence Techniques
6. Fuel Effects on Turbulent Premixed Jet Flame Topology as Resolved by CH PLIF Imaging
7. A Computational Investigation of the Effect of Surface Roughness on the Development of a Liquid Jet in Subsonic Crossflow
8. Characterizing nonequilibrium at the shock front in high-enthalpy shock tube experiments with pure oxygen
9. Exploration of Two-Phase Flow Structures in an Aluminum Nozzle of an Aerated-Liquid Injector Using X-Ray Fluorescence Techniques
10. Supersonic Cavity Flow Control by Upstream Filamentary Plasma
11. Fuel Effects on Turbulent Premixed Jet Flame Topology as Resolved by CH PLIF Imaging
12. Exploration of Two-Phase Flow Structures in Metal Nozzles with Various Configurations Using X-Ray Fluorescence Techniques
13. A Computational Investigation of the Effect of Surface Roughness on the Development of a Liquid Jet in Subsonic Crossflow
14. Effects of Detonation Decoupling on the Ignition of a Supersonic Cavity for Scramjets
15. Exploration of Two-Phase Flow Structures in an Aluminum Nozzle of an Aerated-Liquid Injector Using X-Ray Fluorescence Techniques
16. Characterizing nonequilibrium at the shock front in high-enthalpy shock tube experiments with pure oxygen
17. Supersonic Cavity Flow Control by Upstream Filamentary Plasma
18. Hybrid RANS/LES and kHz-Rate PIV of a Reacting Cavity Flameholder at Mach 3
19. Exploration of Near-Field Cross-Sectional Structures of Aerated-Liquid Jets Using Confocal X-Ray Fluorescence
20. Simultaneous Neutron Radiography of Metal Nozzle Geometry and Near-Field Spray
21. Confocal X-Ray Fluorescence for the Exploration of Near-Field Structures of Aerated-Liquid Jets in Subsonic Crossflows
22. Statistical Measurements of Fuel Mole Fraction in Scramjet Cavity Flameholder with a Fuel Surrogate
23. Quasi-DC Discharge Mixing Enhancement in a Supersonic Combustor with a Cavity-Based Flameholder
24. Control of Amplitude and Position of Reflected Shock Wave by Stripwise Plasma
25. Qualitative Study of Near-Field and Cross-Sectional Structures of Liquid Jets in Supersonic Crossflow
26. The effects of ozonolysis activated autoignition on non-premixed jet flames
27. Cavity-Based Flow Control in A Supersonic Duct Utilizing a Q-DC Plasma Shock Wave Generator
28. Hybrid RANS/LES and kHz-Rate PIV of a Reacting Cavity Flameholder at Mach 3
29. Simultaneous Neutron Radiography of Metal Nozzle Geometry and Near-Field Spray
30. Effect of Magnetic Field on the Quasi-DC Discharge Dynamics in Mach 2 Airflow
31. Confocal X-Ray Fluorescence for the Exploration of Near-Field Structures of Aerated-Liquid Jets in Subsonic Crossflows
32. Statistical Measurements of Fuel Mole Fraction in Scramjet Cavity Flameholder with a Fuel Surrogate
33. Dynamic Response of an Oblique Shock Wave Generated by a Q-DC Discharge in Pulse-Repetitive Mode
34. Structures and Temporal Evolution of Liquid Jets in Supersonic Crossflow
35. The Effect of Ozonolysis Activated Autoignition on Jet Flame Dynamics
36. Digital Holographic Analysis of the Breakup of Aerated Liquid Jets in Supersonic Crossflow
37. Characterization of Transient Operation of a Quasi-DC Electrical Discharge in Supersonic Flow
38. Self-induced transitions between stable and thermoacoustically excited states in a model swirl-stabilized burner at elevated pressure
39. High-Speed Schlieren and 10-Hz Kr PLIF for the new AFRL Mach-6 Ludwieg Tube Hypersonic Wind Tunnel
40. Investigation of Flow and Combustion Dynamics of an Ethylene Transverse Jet in a Model Scramjet
41. Quasi-DC Discharge Mixing Enhancement in a Supersonic Combustor with a Cavity-Based Flameholder
42. The effects of ozonolysis activated autoignition on non-premixed jet flames
43. Cavity-Based Flow Control in A Supersonic Duct Utilizing a Q-DC Plasma Shock Wave Generator
44. Qualitative Study of Near-Field and Cross-Sectional Structures of Liquid Jets in Supersonic Crossflow
45. Derivations of Averaged Two-Phase Flow Properties Using X-Ray Fluorescence Measurements
46. Control of Amplitude and Position of Reflected Shock Wave by Stripwise Plasma
47. On the interactions of an axisymmetric and two precessing modes in a model combustor
48. Single-Shot 3D Flame Imaging Using CH-Based VLIF (Volumetric Laser Induced Fluorescence)
49. 20 kHz 3D measurements in a Mach 2 combustor based on tomographic chemiluminescence
50. The Effect of Ozone Addition on Autoignition and Flame Stabilization
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