A continuous flow liquid propellant strand burner for high pressure monopropellant and bipropellant combustion studies-Reference-Cited by-同舟云学术

A continuous flow liquid propellant strand burner for high pressure monopropellant and bipropellant combustion studies

Published:2021-02-01 Issue:2 Volume:92 Page:025106
ISSN:0034-6748
Container-title:Review of Scientific Instruments
language:en
Short-container-title:Review of Scientific Instruments

Author:

Fuller Casey C.¹,Sinrud Joshua B.²^ORCID,Schwind Rachel A.³^ORCID,Klassen Michael S.¹,Goldsmith C. Franklin³^ORCID,Walker Robert A.²⁴^ORCID

Affiliation:

1. Combustion Science and Engineering, Inc., 8940 Old Annapolis Rd. Suite L, Columbia, Maryland 21045, USA

2. Montana Materials Science Program, Montana State University, Bozeman, Montana 59717, USA

3. Department of Chemical and Environmental Engineering, Brown University, Providence, Rhode Island 02912, USA

4. Department of Chemistry and Biochemistry, Montana State University, Bozeman, Montana 59717, USA

Funder

Office of Naval Research

Publisher

AIP Publishing

Subject

Instrumentation

Link

https://aip.scitation.org/doi/am-pdf/10.1063/5.0022780

Reference21 articles.

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2. Decomposition of nitromethane in shock waves: The primary stage and the kinetics of decomposition at pressures of about 40 atm

3. An experimental and modeling study of nitromethane + O 2 + N 2 ignition in a shock tube

4. Nitromethane ignition behind reflected shock waves: Experimental and numerical study

5. A. Birk, M. McQuaid, and G. Bliesener, “Reacting liquid monopropellant sprays: Experiments with high velocity full cone sprays in 33 MPa, 500 C nitrogen,” Report No. ARL-TR-17, Army Research Laboratory, Aberdeen Proving Ground, MD, 1992.

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3. Experimental study of linear burning rates of liquid nitromethane using a novel high-pressure continuous feed liquid strand burner;Proceedings of the Combustion Institute;2022-11

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