A combustion-driven facility for hypersonic sustained flight simulation
Esposito, Antonio and Lappa, Marcello and Allouis, Christophe (2024) A combustion-driven facility for hypersonic sustained flight simulation. Journal of Aerospace Science, Technologies & Systems, 103 (3). pp. 271-287. ISSN 0365-7442 (https://doi.org/10.1007/s42496-024-00213-9)
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Abstract
This study reports on the development of a new Blowdown-Induction Facility driven by two different Oxygen-Fueled Guns. The facility has been conceived and realized to simulate different flow conditions in the context of hypersonic sustained flight. Here the underlying principles are illustrated critically, along with a focused description of the various facility subsystems, their interconnections and the procedures specifically conceived to overcome some of the technical complexities on which this facility relies. The facility performances are finally presented in relation to some prototype applications, together with an indication of the related limits, advantages and possible directions for future improvements.
ORCID iDs
Esposito, Antonio, Lappa, Marcello ORCID: https://orcid.org/0000-0002-0835-3420 and Allouis, Christophe;-
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Item type: Article ID code: 88462 Dates: DateEvent1 September 2024Published17 April 2024Published Online12 March 2024AcceptedSubjects: Technology > Motor vehicles. Aeronautics. Astronautics > Aeronautics. Aeronautical engineering Department: Faculty of Engineering > Mechanical and Aerospace Engineering
Strategic Research Themes > Ocean, Air and SpaceDepositing user: Pure Administrator Date deposited: 15 Mar 2024 12:31 Last modified: 11 Nov 2024 14:15 URI: https://strathprints.strath.ac.uk/id/eprint/88462