Assessment of the mass flow rate of air in a shock-tunnel direct-connect scramjet combustor

Aerospace Science and Technology 2026 Open access

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Authors: Lucas F. Ribeiro, Pedro A. Matos, Matheus Alvarenga, Dermeval Carinhana, M. A. S. Minucci, Lucas Galembeck, Israel Rêgo
DOI: 10.1016/j.ast.2026.112514
Cited by: 0
References: 22

Fields of Study & Subjects

Gas Dynamics and Kinetic Theory Plasma and Flow Control in Aerodynamics Computational Fluid Dynamics and Aerodynamics

Publication details

Journal / source
Aerospace Science and Technology
Publisher
Elsevier BV
Volume
176
Pages
112514–112514
Publication date
5 May 2026
Language
EN