@inproceedings{0057e8e105da44ffa165df4a2be367f1,
title = "Adaptive finite element analysis of shock-induced combustion",
abstract = "An adaptive finite element method for a numerical parametric study is presented to simulate shockinduced combustion with a variation in freestream conditions and projectile radii. The three cases have been simulated for Machs 4.18, 5.11, and 6.46 with a projectile diameter of 15 mm. Machs 4.18 and 5.11 show an unsteady reaction front, whereas Mach 6.46 represents a steady reaction front. However, Mach 4.18, the case for the Mach number below the Chapman-Jouguet can also lead to a stable reaction front by reducing radius of the projectile. Thus, Chapman-Jouguet speed and the projectile radius are crucial factors for the instabilities to trigger.",
keywords = "Bow Shock, Finite Element Method, Induction Zone, Mixed Explicit Implicit method, Reaction Front",
author = "Suyeon Moon and Chooungwon Lee and Changhyun Sohn",
year = "2002",
doi = "10.2514/6.2002-3857",
language = "English",
isbn = "9781624101151",
series = "38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit",
note = "38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2002 ; Conference date: 07-07-2002 Through 10-07-2002",
}