Parametric study of combustor and nozzle design for quasi-axisymmetric scramjet engines

Translated title of the contribution: Parametric study of combustor and nozzle design for quasi-axisymmetric scramjet engines

Katsuyoshi Tanimizu, Trent Jones, Hideaki Ogawa, Adrian Pudsey

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Translated title of the contributionParametric study of combustor and nozzle design for quasi-axisymmetric scramjet engines
Original languageUndefined/Unknown
Title of host publication8th Asia-Pacific International Symposium on Aerospace Technology (APISAT 2016)
Publication statusPublished - Oct 2016

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