Characterization of supersonic mixing in a nonreacting Mach 2 combustor

Author:

HOLLO STEVEN1,MCDANIEL JAMES1,HARTFIELD, JR. ROY1

Affiliation:

1. Virginia, University, Charlottesville

Publisher

American Institute of Aeronautics and Astronautics

Reference22 articles.

1. Jan. 1983;McDaniel J.C.

2. McDaniel, J.C. "InvestigationofLaser-InducedIodine Fluorescence for the Measurement of Density in Compressible Flows,'' Ph.D. Dissertation,Stanford Univ., Jan. 1982.

3. Laser-induced iodine fluorescence technique for quantitative measurement in a nonreacting supersonic combustor

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1. Enhanced Mixing in Supersonic Flow Using a Pulse Detonation Combustor;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

2. Pulsed Detonation Combustor in a Supersonic Cross-Flow for Enhanced Mixing and Ignition;41st AIAA Fluid Dynamics Conference and Exhibit;2011-06-14

3. Flow patterns and mixing characteristics of gaseous fuel multiple injections in a non-reacting supersonic combustor;Heat and Mass Transfer;2011-04-30

4. Design and Testing of Clover Nozzle;14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference;2006-06-15

5. Velocity Measurements of a Jet Injected into a Supersonic Crossflow;Journal of Propulsion and Power;1997-03

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