Effect of Particle Orientation on the Burning Rate of Ammonium-Perchlorate-Based Solid Propellants
Author:
Publisher
Pleiades Publishing Ltd
Subject
General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry
Link
https://link.springer.com/content/pdf/10.1134/S0010508221060071.pdf
Reference16 articles.
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2. T. L. Jackson and J. Buckmaster, “Heterogeneous Propellant Combustion," AIAA J. 40 (6), 1122–1130 (2002); DOI: 10.2514/2.1761.
3. L. Massa, T. L. Jackson, and M. Short, “Numerical Solution of Three-Dimensional Heterogeneous Solid Propellants," Combust. Theory Model. 7 (3), 579–602 (2003); DOI: 10.1088/1364-7830/7/3/308.
4. D. Deepak, R. Jeenu, P. Sridharan, and M. S. Padmanabhan, “Direct Evidence of Spatial Burning Rate Variation as Cause of Midweb Anomaly," J. Propul. Power 17 (2), 449–452 (2001); DOI: 10.2514/2.5763.
5. T. E. Kallmeyer and L. H. Sayer, “Differences between Actual and Predicted Pressure–Time Histories of Solid Rocket Motors," in 18th AIAA/SAE/ASME Joint Propul. Conf., Cleveland, Ohio, July 21–23, 1982, AIAA Paper No. 1982-1094; DOI: 10.2514/6.1982-1094.
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