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Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle — ReaderExpo

Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle

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Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle

by Timothy W. Simpson

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Aerospike enginesKrigingRocket nozzlesPropulsion system configurationsMultidisciplinary design optimizationDesign analysis

Keep the story going

High-speed observer

T. J. Rieckhoff

The control system for the X-33 linear aerospike engine

Jerry E. Jackson

An inviscid computational study of an X-33 configuration at hypersonic speeds

Book

An inviscid computational study of an X-33 configuration at hypersonic speeds

Ramadas K. Prabhu

Automated testing experience of the linear aerospike SR-71 experiment (LASRE) controller

Richard R. Larson

Analysis of aerospike plume induced base-heating environment

T.-S Wang