A simplified design and optimization method of aerospike nozzle contour and the results of tests and numerical simulation of aerospike nozzles are presented. advantages of the aerospike nozzle is the ability to achieve thrust vectoring aerodynamically Figure 1 compares two aerospike-based nozzle designs to their. design strategy. Introduction. A multidisciplinary analytic model of a linear aerospike rocket nozzle has been developed; this model includes predictions.

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Salas and Herbert Dunn and Natalia M. Alexandrov Published A model of a linear aerospike rocket nozzle that consists of coupled aerodynamic and structural analyses has been developed.

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A nonlinear computational fluid dynamics code is used to calculate the aerodynamic thrust, and a three-dimensional finite-element model is used to determine the structural response and weight. From This Paper Figures, tables, and topics from this paper.


Multidisciplinary design optimization Search for additional papers on this topic. Topics Discussed in This Paper.

Multidisciplinary design optimization Aerospike Database Computational fluid dynamics. Nozzle Device Component Nonlinear system Mathematical optimization.

Citations Publications citing this paper. Showing of 8 extracted citations.

Multidisciplinary Approach to Aerospike Nozzle Design

MunakataShigeru Sato TorrezDerek J. DalleJames F.

SimpsonTimothy M. MaueryJohn J.

KorteFarrokh Mistree PadulaJohn J. KorteHerbert DunnA.

Multidisciplinary Approach to Aerospike Nozzle Design – Semantic Scholar

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