@inproceedings{a3936430ffa442719c147d10bd68fe1e,
title = "Experimental Measurements of Hypersonic Boundary Layer Transition on the STORT Ogive Geometry",
abstract = "Experiments were performed to investigate hypersonic boundary layer transition on a scaled STORT ogive model in the Mach 5 Ludwieg Tube at the University of Arizona. The freestream unit Reynolds number of these tests ranged from 5.33 ×106 /m to 23.4 ×106 /m. Instrumentation and optical diagnostics included pressure sensors, infrared thermography and high speed schlieren to investigate the primary transition mechanism. Transition onset was observed from the wall heat flux distribution for all except the lowest unit Reynolds number. It appears from the pressure data and schlieren that transition is dominated by first mode instability. The frequency of these instabilities agreed with linear stability theory calculations.",
author = "Ranjini Ramesh and Adam Skora and Christoph Hader and Hermann Fasel and Stuart Craig",
note = "Publisher Copyright: {\textcopyright} 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Aviation Forum and ASCEND, 2024 ; Conference date: 29-07-2024 Through 02-08-2024",
year = "2024",
doi = "10.2514/6.2024-4152",
language = "English (US)",
isbn = "9781624107160",
series = "AIAA Aviation Forum and ASCEND, 2024",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Aviation Forum and ASCEND, 2024",
}