Physical insight into axisymmetric scramjet intake design via multi-objective design optimization using surrogate-assisted evolutionary algorithms

Author:

Fujio ChihiroORCID,Ogawa HideakiORCID

Funder

Japan Society for the Promotion of Science

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Reusable launch of small satellites using scramjets;Preller;J. Spacecr. Rockets,2017

2. Trajectory design of a rocket-scramjet-rocket multistage launch system;Forbes-Spyratos;J. Spacecr. Rockets,2019

3. Flight data analysis of the HyShot 2 scramjet flight experiment;Smart;AIAA J.,2006

4. X-43 - Scramjet Power Breaks the Hypersonic Barrier: Dryden Lectureship in Research for 2006;Mcclinton,2006

5. Physical insight into fuel-air mixing characteristics for upstream-fuel injected scramjets via multi-objective design optimization;Ogawa;J. Propuls. Power,2015

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