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Numerical Method to Estimate Thermal Conductivity of a Model Composite Propellant
Published in American Institute of Aeronautics and Astronautics
2016
DOI: 10.2514/6.2016-4597
Abstract is unavailable for this paper.
Topics: Propellant (58)%58% related to the paper, Composite number (55)%55% related to the paper and Thermal conductivity (53)%53% related to the paper
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About the journal
| Publisher | Data powered by TypesetAmerican Institute of Aeronautics and Astronautics |
|---|---|
| ISSN | 0001-1452 |
| Impact Factor | 1.868 |
| Open Access | No |
| Citation Style | unsrt |
| Sherpa RoMEO Archiving Policy | Green |
Authors (1)
Periyapatna A. Ramakrishna- Effect of protrusion on the enhancement of regression rate
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