Work

Quasi-Direct-Connect Scramjet Combustor Experiments in the X3R Shock Tunnel Using T4’s Mach 4 Nozzle

Year: 2025

Type: conference-paper

DOI: 10.2514/6.2025-3048

Authors: Matthew A. Trudgian, Will Landsberg, Richard Morgan, Ananthanarayanan Veeraragavan, Daniel R. Smith, Damian R. Curran, Samuel J. Stennett, Kalon Heintze, Wilson Chan

Institutions: The University of Queensland, Defence Science and Technology Group

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4412485201

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