NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A single mode approximation in the solution of nonlinear combustion instability problemsNonlinear combustion stability problems in liquid propellant rocket engines, describing unsteady combustion response by Crocco time lag hypothesis
Document ID
19710050774
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Powell, E. A.
Zinn, B. T.
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Subject Category
Propulsion Systems
Accession Number
71A31471
Funding Number(s)
CONTRACT_GRANT: NGR-11-002-083
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available