NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Numerical solutions of several reflected shock-wave flow fields with nonequilibrium chemical reactionsThe method of characteristics for a chemically reacting gas is used in the construction of the time-dependent, one-dimensional flow field resulting from the normal reflection of an incident shock wave at the end wall of a shock tube. Nonequilibrium chemical reactions are allowed behind both the incident and reflected shock waves. All the solutions are evaluated for oxygen, but the results are generally representative of any inviscid, nonconducting, and nonradiating diatomic gas. The solutions clearly show that: (1) both the incident- and reflected-shock chemical relaxation times are important in governing the time to attain steady state thermodynamic properties; and (2) adjacent to the end wall, an excess-entropy layer develops wherein the steady state values of all the thermodynamic variables except pressure differ significantly from their corresponding Rankine-Hugoniot equilibrium values.
Document ID
19720021582
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hanson, R. K.
(NASA Ames Research Center Moffett Field, CA, United States)
Presley, L. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Williams, E. V.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-6885
A-4226
Report Number: NASA-TN-D-6885
Report Number: A-4226
Accession Number
72N29232
Funding Number(s)
PROJECT: RTOP 117-07-04-13-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available