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NASA NTRS · 19650042666

Combustion process influence on stability.

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Abstract

Rocket engine combustion process influence on stability, vaporization, atomization and growth disturbances

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COMBUSTION STABILITY ROCKET COMBUSTOR DISTURBANCE THEORY

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Priem, R. J.. 1965-05-01. Combustion process influence on stability.. https://ntrs.nasa.gov/citations/19650042666

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