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A study of high frequency nonlinear combustion instability in baffled annular liquid propellant rocket motorsComputer program contains mathematical model which provides relationship between engine gas dynamics and combustion processes. Mathematically simulated explosions initiate gas disturbances. Design methods for damping disturbances can be studied to prevent future engine shutdown or destruction.
Document ID
19710000523
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Abreu, A.
Burstein, S. Z.
Kushida, R. O.
Schechter, H.
Date Acquired
August 6, 2013
Publication Date
December 1, 1971
Subject Category
Mathematics And Information Sciences
Report/Patent Number
NPO-11800
Report Number: NPO-11800
Accession Number
71B10532
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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