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
01.11.1973
Sonstige
Keine Angabe
Englisch
Fluidic nozzle throats in solid rocket motors
TIBKAT | 2019
|BOUNDARY-LAYER MEASUREMENTS AT SUPERSONIC NOZZLE THROATS
NTRS | 1956
|