Concepedia

Effect of chamber pressure, flow per element, and contraction ratio on acoustic-mode instability in hydrogen-oxygen rockets

C. E. Feiler, C. J. Morgan, J. P. Wanhainen

NASA Technical Reports Server (NASA) · 1968 · 37 citations · 2 references

Open access

Concepts

Natural SciencesMechanical EngineeringPhysicsAcousticsFluid DynamicsInternal Combustion EnginesAcoustic Wave PropagationAeroacousticsEngine DesignRocket PropulsionAcoustic InstabilitiesChamber Pressure EffectsChamber Pressure OptimizationChamber Pressure ProfilingDynamic Pressure EffectsHydrogen Internal Combustion EnginesRocket Combustion Instability

Abstract

Chamber pressure, contraction ratio, and flow per element effects on acoustic mode instability in hydrogen oxygen engines

References

2

Analysis of frequency response characteristics of propellant vaporization

M. F. Heidmann, P. R. Wieber · NASA Technical Reports Server (NASA) · 1966 · 52 citations · Full text

Engineering, Mechanical Engineering, Physics +11

Dynamic response of gaseous-hydrogen flow system and its application to high-frequency combustion instability

C. E. Feiler, M. F. Heidmann · NASA Technical Reports Server (NASA) · 1967 · 47 citations · Full text

Engineering, Chemical Engineering, Mechanical Engineering +17