A general method for determining optimum thrust nozzle contours for gas-particle flows.
Optimization analysis for axisymmetric rocket motor nozzle design based on assumptions for gas particle flow
GAS FLOW↗
Engineering topics
Hoffman, J. D.
Publications and source records attributed to Hoffman, J. D..
A general method for determining optimum thrust nozzle contours for chemically reacting gas flows.
Optimum thrust nozzle contours for chemically reacting gas flows, obtaining set of partial differential equations for gas dynamic properties
GAS DYNAMICS↗
Optimum thrust nozzle contours for chemically reacting gas flows
Supersonic rocket nozzle design for optimum thrust with chemically reacting gas flows
GAS FLOW↗