@inproceedings{3fad52731b0d49b6bae7ff888ff8ce6c,
title = "Hypersonic Aerodynamic Characterization of a Winged Body Re-entry Configuration Using Chemical Non-Equilibrium CFD Simulations",
abstract = "Hypersonic aerodynamic characterization in presence of high temperature effects is essential for orbiter re-entry for winged body configuration. CFD studies with chemical non- equilibrium solver are carried out for aerodynamic characterization. Validation of the methodology is done by simulating hypersonic pitching moment anomaly of space shuttle orbiter. Aerodynamic data for 6≤M≤23 is obtained for winged body configuration and high temperature effects are analyzed for basic and elevon deflected configuration.",
author = "{Nagpa L}, Ankur and G. Vidya and Patil, {M. M.} and V. Ashok",
note = "Publisher Copyright: {\textcopyright} 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2023 ; Conference date: 28-05-2023 Through 01-06-2023",
year = "2023",
doi = "10.2514/6.2023-3083",
language = "English",
isbn = "9781624107108",
series = "25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2023",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2023",
}