THERMAL SCIENCE

International Scientific Journal

Ognjen V. Ognjanović

,

Stevan M. Maksimović

,

Nenad D. Vidanović

,

Stevo D. Šegan

,

Gordana M. Kastratović

NUMERICAL AERODYNAMIC-THERMAL-STRUCTURAL ANALYSES OF MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT CONDITIONS

ABSTRACT
Attention in this work is focused on aerodynamic heating and aero-thermo-mechanical analysis of fin type structures on the missile at supersonic flight. At high Mach number the heat due to friction between body and flow, i.e. viscous heating must be taken into account because the velocity field is coupled with the temperature field. The flow field around the fins of the missile and especially the temperature distribution on its surface, as well as aerodynamic-thermal-structural analyses are numerically modeled in ANSYS Workbench environment. The investigation was carried out for two Mach numbers (M = 2.3 and M = 3.7). Own available structural experimental results have been used for computational structural mechanics (CSM) validation and verification, in order to assure credibility of numerical fluid-thermal-structure interaction (FTSI). Conducted simulations were carried out to better understand the FTSIs of the missile fin during supersonic flight.
KEYWORDS
missile fins, supersonic flight, aerodynamic heating, fluid-thermal-structure interaction
PAPER SUBMITTED: 2016-09-19
PAPER REVISED: 2016-11-11
PAPER ACCEPTED: 2016-11-29
PUBLISHED ONLINE: 2017-01-14
DOI REFERENCE: https://doi.org/10.2298/TSCI160919318O
CITATION EXPORT: view in browser or download as text file
THERMAL SCIENCE YEAR 2017, VOLUME 21, ISSUE Issue 6, PAGES [3037 - 3049]
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Numerical aerodynamic-thermal-structural analyses of missile fin configuration during supersonic flight conditions

© 2024 Society of Thermal Engineers of Serbia. Published by the Vinča Institute of Nuclear Sciences, National Institute of the Republic of Serbia, Belgrade, Serbia. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution-NonCommercial-NoDerivs 4.0 International licence