A physico-mathematical model of rocket exhaust plumes
- 31 March 1997
- journal article
- Published by Elsevier in International Journal of Heat and Mass Transfer
- Vol. 40 (5) , 1227-1241
- https://doi.org/10.1016/0017-9310(96)00140-8
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Influence of Chemical Kinetics and Unmixedness on Burning in Supersonic Hydrogen FlamesAIAA Journal, 1980
- Vibrational nonequilibrium radiation in diatomic gases—IInternational Journal of Heat and Mass Transfer, 1978
- Effect of crystallization kinetics on rocket performanceAIAA Journal, 1977
- Effects of nonequilibrium chemistry on electrical properties of solid propellant rocket exhaust plumesCombustion and Flame, 1971
- Finite difference methods of solution of the boundary-layer equationsAIAA Journal, 1970
- Numerical computation of steady, supersonic, two-dimensional gas flow in natural coordinatesJournal of Computational Physics, 1969
- Quenching of excited hydroxyl (2Σ+, υ′ = 0) radicals in flamesJournal of Quantitative Spectroscopy and Radiative Transfer, 1967
- Particle drag and heat transfer in rocket nozzlesAIAA Journal, 1964
- Abnormal Excitation of OH in H2/O2/N2 FlamesThe Journal of Chemical Physics, 1959
- Electronic Quenching of OH(2Σ+) in Flames and Its Significance in the Interpretation of Rotational RelaxationThe Journal of Chemical Physics, 1959