An investigation of supersonic mixing mechanisms for the chemical oxygen-iodine laser (COIL)
Author:
Affiliation:
1. USAF, Research Lab., Kirtland AFB, NM
2. Logicon, Albuquerque, NM
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-3429
Reference18 articles.
1. Phillips Laboratory COIL technology overview
2. A detailed comparison of a computational fluid dynamic simulation and a laboratory experiment for a COIL laser
3. A simplified analytic model for gain saturation and power extraction in the flowing chemical oxygen-iodine laser
4. 7*10-" 6.7*10-12 1.6*10-" 4.0*10- 6.0*10-`* 8.0-lO-2' 4.0*10-12 1.6*10-" 7.0*lo-`5 3.8.10-" 3.0*10-10 5.0*10-" 3.0*10-
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1. Mixing in a supersonic COIL laser: influence of trip jets;Experiments in Fluids;2010-08-05
2. Numerical Simulation on Supersonic-Flow Chemical Oxygen-Iodine Laser Adopting High Mach-Number Ramp-Nozzle Array;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2007
3. PLIF Visualization and Quantitative Mixing Measurements of a Supersonic Injection Nozzle;37th AIAA Plasmadynamics and Lasers Conference;2006-06-05
4. Numerical Simulation of Q-Switched Supersonic Flow Chemical Oxygen-Iodine Laser by Solving Time-Dependent Paraxial Wave Equation;JSME International Journal Series B;2006
5. PLIF Flow Visualization of a Supersonic Injection COIL Nozzle;36th AIAA Plasmadynamics and Lasers Conference;2005-06-06
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