Engineering topics
Publications and source records attributed to Stromsta, R. R..
Digital computer program computes and analyzes supersonic flow field in axisymmetric rocket nozzle for specified gas properties, nozzle geometry, and input or starting line. Method of characteristics is used for solution of set of hyperbolic partial differential equations.
Analytical evaluation of secondary flow injection effects on rocket engine performance including cold flow and simulated hot flow data
Aerobell extendible nozzle rocket engine design and performance, cold flow and simulated hot flow test results
Analytical evaluation of secondary flow injection effects on rocket engine performance including cold flow and simulated hot flow data
Aerobell extendible nozzle rocket engine design and performance, cold flow and simulated hot flow test results