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Nonlinear combustion instability in liquid- propellant rocket enginesLiquid propellant rocket engine combustion instabilities, describing unsteady combustor flow by single nonlinear wave equation with stable and unstable finite amplitude limit cycles
Document ID
19700068309
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Powell, E. A.
Zinn, B. T.
Date Acquired
August 5, 2013
Publication Date
August 1, 1970
Subject Category
Propulsion Systems
Meeting Information
Meeting: COMBUSTION INST., INTERNATIONAL SYMPOSIUM ON COMBUSTION, 13TH, U. OF UTAH
Location: SALT LAKE CITY, UT
Start Date: August 23, 1970
End Date: August 29, 1970
Sponsors: COMBUSTION INST.
Accession Number
70A44425
Funding Number(s)
CONTRACT_GRANT: NGL-11-002-085
Distribution Limits
Public
Copyright
Other

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