Effect of flameholding cavity geometry on the flowfield of a solid fuel scramjet-Reference-Cited by-同舟云学术

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Effect of flameholding cavity geometry on the flowfield of a solid fuel scramjet

Published:2024-11 Issue: Volume:224 Page:508-519
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Prokesch Youri^ORCID,Duran Abram,Gallegos Dominic^ORCID,Schlussel Ethan,Young Gregory

Funder

Office of Naval Research

Publisher

Elsevier BV

Reference32 articles.

1. Mechanics and Thermodynamics of Propulsion;Hill,1992

2. Investigation into the feasibility of using solid fuel ramjets for high supersonic/low hypersonic tactical missiles, MS;Witt;Naval Postgraduate School,1989

3. Investigation of a solid fuel scramjet combustor;Ben-Yakar;J. Propul. Power,1998

4. Turbulent boundary layer combustion in the hybrid rocket;Marxman;Symposium (International) on Combustion,1963

5. Research progress on strut-equipped supersonic combustors for scramjet application;Chang;Prog. Aero. Sci.,2018

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