Concepedia

Effect of injection element radial distribution and chamber geometry on acoustic mode instability in a hydrogen oxygen rocket

C. J. Morgan, J. P. Wanhainen

NASA Technical Reports Server (NASA) · 1969 · 31 citations · 3 references

Open access

Concepts

AeroacousticsAcoustic Mode InstabilityHydrogen Oxygen EnginesEngineeringAerospace EngineeringInjector Radial DistributionChamber GeometryRocket EngineIn-cylinder FlowUnderwater ExplosionAerospace Propulsion SystemsPropulsionAerospace PropulsionHydrogen Oxygen RocketFuel Injection

Abstract

Injector radial distribution and thrust chamber geometry effect on acoustic mode instability in hydrogen oxygen engines

References

3

<i>The Theory of Sound</i>

Lord Rayleigh, Norman H. Nachtrieb · Physics Today · 1957 · 3.5K citations

Music, Acoustics, Psychoacoustics +1

BEHAVIOR OF SUPERCRITICAL NOZZLES UNDER THREE-DIMENSIONAL OSCILLATORY CONDITIONS

L. CROCCO, William A. Sirignano · Defense Technical Information Center (DTIC) · 1967 · 13 citations

Combustion instability with finite mach number flow and acoustic liners

Richard J. Priem, Edward J. Rice · Symposium (International) on Combustion · 1969 · 11 citations

Aeroacoustics, Unsteady Flow, Compressible Flow +9