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TAS::57 3600::TAS "HIGH-PRESSURE LIQUID-PROPELLANT ROCKET ENGINE COMBUSTION INSTABILITY: COMPLEX SYSTEM, BASIS MODELING"

$939,395FY2015Department of DefenseDOD

University Of California Irvine, Irvine CA

Investigators

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TAS::57 3600::TAS "HIGH-PRESSURE LIQUID-PROPELLANT ROCKET ENGINE COMBUSTION INSTABILITY: COMPLEX SYSTEM, BASIS MODELING" · GrantIndex