The research program was concerned with (1) the problem of high frequency longitudinal pressure oscillations in premixed gaseous propellant combustors and (2) the steady-state and stability operating characteristics of bi-phase propellant rocket combustors operating at sub-critical conditions. Both analytical and experimental work were performed in order to study the aforementioned problems. (Author)
Parametric Study of Rocket Instability
1968
8 pages
Report
No indication
English