Thermal compression effects within a fundamental, hydrogen-fuelled scramjet-Reference-Cited by-同舟云学术

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Thermal compression effects within a fundamental, hydrogen-fuelled scramjet

Published:2021-03 Issue: Volume:110 Page:106499
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Vanyai Tristan^ORCID,Brieschenk Stefan,Bricalli Mathew,Sopek Tamara,McIntyre Timothy J.^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

1. Design Considerations for Combined Air Breathing-Rocket Propulsion Systems;Kors,1990

2. Orbital delivery of small payloads using hypersonic airbreathing propulsion;Smart;J. Spacecr. Rockets,2009

3. Design of an airbreathing second stage for a rocket-scramjet-rocket launch vehicle;Jazra;J. Spacecr. Rockets,2013

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

5. Preliminary Investigation of Supersonic Diffusers;Kantrowitz,1945

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1. The effect of leading edge bluntness on scramjet performance;Aerospace Science and Technology;2024-03

2. Prospects for scramjet engines in reusable launch applications: A review;International Journal of Hydrogen Energy;2023-11

3. Review of the Role of Geometrical Modification of Scramjet Combustor on Performance Characteristics;Materials and Technologies for a Green Environment;2023-03-21

4. A coupling study of ignition position on fuel-air mixing and diffusion of a linear hydrogen engine;International Journal of Hydrogen Energy;2022-11

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