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NASA NTRS · 19660061818

Design of optimized three-dimensional nozzles.

Murthy, S. N. B.·Thompson, H. D.

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Abstract

Optimization of supersonic portion of three- dimensional flow geometry in rocket motor nozzle for maximum thrust

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THREE-DIMENSIONAL FLOW OPTIMUM THRUST PROGRAMMING SUPERSONIC NOZZLE ROCKET NOZZLE NOZZLE FLOW

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Murthy, S. N. B., Thompson, H. D.. 1966-09-01. Design of optimized three-dimensional nozzles.. https://ntrs.nasa.gov/citations/19660061818

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