DTIC ADA041530: Propulsion Nozzle Studies. Volume II. Design of Maximum Thrust Nozzle-Base-Boattail Contours.Reportar como inadecuado



 DTIC ADA041530: Propulsion Nozzle Studies. Volume II. Design of Maximum Thrust Nozzle-Base-Boattail Contours.


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A production-type computer program was developed for the design of maximum thrust axisymmetric nozzle-base-boattail contours. The flow field analysis is based on the governing equations for the rotational flow of a frozen or equilibrium gas mixture. The contour optimization is based on the direct optimization of a nonlinear function of several (thr

Autor: Defense Technical Information Center

Fuente: https://archive.org/







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