Experimental study of nonequilibrium expanding flows has been carried out by measuring static pressure at several axial locations in 30° included angle conical nozzle attached to reflected end of combustion driven shock tube; data reduction procedures employed are described and methods for treating effects due to boundary-layer growth on nozzle walls and on static-pressure probe, static-pressure probe size, flow gradients in nozzle, etc, outlined; it has been found that corrections for these effects are necessary to interpret properly static-pressure data.
Experimental study of nonequilibrium expanding flows
AIAA J
AIAA Journal ; 3 , n 2
1965
8 pages
Aufsatz (Zeitschrift)
Englisch
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Experimental study of nonequilibrium expanding flows
AIAA | 1965
|Experimental study of nonequilibrium expanding flows
AIAA | 1964
|