NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
Swirling flow through multiple nozzlesSwirling flow through multiple nozzles of simulated solid propellant rocket motors, determining thrust and mass flow effects on passage
Document ID
19710030895
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Essing, J. E.
Sforzini, R. H.
Date Acquired
August 6, 2013
Publication Date
November 1, 1970
Subject Category
Fluid Mechanics
Accession Number
71A11592
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available