A theory is presented that makes it possible to apply one-dimensional techniques to compressible striated nozzle flow with small radius of curvature ratio throats. The throat plane solution is shown to approximate the two-dimensional axisymmetric flowfield and can be used for analyzing the throat plane in converging-diverging type nozzles with striated flow for radius of curvature throat ratios down to 0.25.
Striated nozzle flow with small radius of curvature ratio throats
1973-11-01
Miscellaneous
No indication
English
Fluidic nozzle throats in solid rocket motors
TIBKAT | 2019
|BOUNDARY-LAYER MEASUREMENTS AT SUPERSONIC NOZZLE THROATS
NTRS | 1956
|