Experimental supersonic hydrogen combustion employing staged injection behind a rearward-facing step-Reference-Cited by-同舟云学术

Experimental supersonic hydrogen combustion employing staged injection behind a rearward-facing step

Published:1993-05 Issue:3 Volume:9 Page:472-478
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Abbitt John D.,Segal Corin,McDaniel James C.,Krauss Roland H.,Whitehurst Robert B.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference10 articles.

1. Numerical predictions of a rearward-facing-step flow in a supersoniccombustor

2. Mole-fraction imaging of transverse injection in a ducted supersonicflow

3. Planar temperature measurement in compressible flows using laser-induced iodine fluorescence

4. 5Abbitt, J. D., Ill, "Flow Visualization of Supersonic Flow Through a Combustor Section," Ph.D. Dissertation,Univ. of Virginia, Charlottesville, VA, 1991.

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