NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design of Axisymmetric Exhaust Nozzles by Method of Characteristics Incorporating a Variable Isentropic ExponentLimitations on fully developed laminar flows due to compressibility and property variations are examined. The cases, for liquids and for gases, wherein such motions are "exact" are determined and solutions are given. For more general conditions, not permitting an exact fully developed flow, limitations are set. Two cases arise depending on the size of the temperature variation across the channel. Both the forced and free flow are solved for the case of large temperature variation. Finally, there are described briefly some circumstances under which streamwise variations of velocity occur. The case where the velocity varies inversely with the square root of the distance is solved.
Document ID
19980232191
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Guentert, Eleanor Costilow
(NASA Lewis Research Center Cleveland, OH United States)
Neumann, Harvey E.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1959
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TR-R-33
Report Number: NASA-TR-R-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available