@inproceedings{a582195053484e8ab82867f5dc36afd6,
title = "Computation of HyShot scramjet flows in the T4 experiments",
abstract = "Numerical simulations of the HyShot scramjet flows in the T4 shock tunnel experiments are carried out. In order to realistically determine the freestream conditions in the test section, the nozzle flow is calculated by a thermochemical nonequilibrium axisymmetric flow solver. Using the obtained freestream conditions, a flow for the HyShot scramjet model is calculated. The results are compared with the experimental data and the CFD calculated results using the nominal freestream conditions, which are deduced under the thermal equilibrium assumption.",
author = "Michiko Furudate and Lee, {Bok Jik} and Jeung, {In Seuck}",
year = "2005",
language = "English (US)",
isbn = "1563477297",
series = "A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference",
pages = "1419--1428",
booktitle = "A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference",
note = "13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference ; Conference date: 16-05-2005 Through 20-05-2005",
}