SURVEY ON BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT

Saddam Hussain; Anil Verma; Priyanka Jhawar; Dr. G.R.Selokar

SURVEY ON BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT

August 2019

Vol-5, Issue-4

Paper ID: 10686

ISSN: 2395-4396

Downloads: 0

Abstract & Details

Research Area

MECHANICAL ENGINEERING

Keywords

Missile Fins1 Supersonic Flight2 Thermodynamic Heating3 and Thermal-Surface Interaction 4

Abstract

The focus of this paper is to study of heating and thermo-Structural analysis of fin of a missile structures at supersonic flight. The heat due to friction at high Mach number between the flow and body, i. e. viscous heating must be taken into account due to 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 thermal-structural analyses are numerically modeled in ANSYS FLUENT.,

License

This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.

Author Information

#	Name	Institute / Affiliation
1	Saddam Hussain	Department of Mechanical Engineering, SOE, SSSUTMS, M.P., INDIA
2	Anil Verma	Department of Mechanical Engineering, SOE, SSSUTMS, M.P., INDIA
3	Priyanka Jhawar	Department of Mechanical Engineering, SOE, SSSUTMS, M.P., INDIA
4	Dr. G.R.Selokar	Department of Mechanical Engineering, SOE, SSSUTMS, M.P., INDIA

How to Cite

Use the following formats to cite this article in your research.

APA Style

Hussain, Saddam, Verma, Anil, Jhawar, Priyanka, & G.R.Selokar, Dr. (2019). SURVEY ON BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT. International Journal of Advance Research and Innovative Ideas In Education, 5(4), 915-919.

MLA Style

Hussain, Saddam, et al. "SURVEY ON BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT." International Journal of Advance Research and Innovative Ideas In Education, vol. 5, no. 4, 2019, pp. 915-919.

IEEE Style

Saddam Hussain, Anil Verma, Priyanka Jhawar, and Dr. G.R.Selokar, "SURVEY ON BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT," International Journal of Advance Research and Innovative Ideas In Education, vol. 5, no. 4, pp. 915-919, 2019.

Vancouver Style

Hussain Saddam, Verma Anil, Jhawar Priyanka, G.R.Selokar Dr.. SURVEY ON BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT. International Journal of Advance Research and Innovative Ideas In Education. 2019;5(4):915-919.

Harvard Style

Hussain, Saddam, Verma, Anil, Jhawar, Priyanka, & G.R.Selokar, Dr. (2019) 'SURVEY ON BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT', International Journal of Advance Research and Innovative Ideas In Education, 5(4), pp. 915-919.

Chicago Style

Hussain, Saddam, et al. "SURVEY ON BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT." International Journal of Advance Research and Innovative Ideas In Education 5, no. 4 (2019): 915-919.

Turabian Style

Hussain, Saddam, et al. "SURVEY ON BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT." International Journal of Advance Research and Innovative Ideas In Education 5, no. 4 (2019): 915-919.