Gas composition and temperature measurements in a rocket engine combustor using the Raman technique
- 10 January 1994
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Multi-phase simulations of coaxial injector combustionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Numerical analysis of SSME preburner injector atomization and combustion processesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- A calculation procedure for heat, mass and momentum transfer in three-dimensional parabolic flowsInternational Journal of Heat and Mass Transfer, 1972