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
Bell nozzle kernel analysis programBell Nozzle Kernel Analysis Program computes and analyzes the supersonic flowfield in the kernel, or initial expansion region, of a bell or conical nozzle. It analyzes both plane and axisymmetric geometrices for specified gas properties, nozzle throat geometry and input line.
Document ID
19690000146
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Elliot, J. J.
Stromstra, R. R.
Date Acquired
August 5, 2013
Publication Date
May 1, 1969
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MFS-18456
Report Number: MFS-18456
Accession Number
69B10146
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

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