A theoretical model for predicting aluminum oxide particle size distributions in rocket exhausts.
- 1 January 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (1) , 92-98
- https://doi.org/10.2514/3.3389
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- COMBUSTION OF METALSAIAA Journal, 1963
- COMBUSTION STUDIES OF SINGLE ALUMINUM PARTICLESPublished by Elsevier ,1963