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NASA NTRS · 19670060146

Optimum thrust-nozzle contours for gas-particle flows.

Hoffman, J. D.·Thompson, H. D.

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Abstract

Optimization analysis for axisymmetric rocket motor nozzle design based on assumptions for gas particle flow

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DIFFERENTIAL EQUATION GAS FLOW OPTIMIZATION ROCKET NOZZLE NOZZLE GEOMETRY

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Hoffman, J. D., Thompson, H. D.. 1967-10-01. Optimum thrust-nozzle contours for gas-particle flows.. https://ntrs.nasa.gov/citations/19670060146

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