INVESTIGATION OF BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT

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

INVESTIGATION OF BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT

August 2019

Vol-5, Issue-4

Paper ID: 10740

ISSN: 2395-4396

Downloads: 0

Abstract & Details

Research Area

MECHANICAL ENGINEERING

Keywords

Missile Fins1 Supersonic Flight2 Thermodynamic Heating3 Fluid-Thermal-Surface Interaction4 .

Abstract

The investigation was carried out for two Mach numbers (M = 2.5 and M = 3.0 With Alpha 0, 2,5,10 at an Altitude of 5km). And the data are compared with own available Thermal and structural experimental results have been used for computational structural mechanics validation and verification, in order to assure credibility of numerical fluid-thermal-structure interaction. Conducted simulations were carried out to better understand the fluid-thermal-structure interaction of the missile fin during supersonic flight. The fin is modeled in SOLID WORKS and then it is imported in POINTWISE for meshing and then the meshed file is imported to ANSYS FLUENT for solution and Microsoft Excel used for post processing. To this end, a procedure is adopted in which shock-expansion theory is used to predict the flow properties over the fin, with the Eckert reference temperature method then being used to predict the heat transfer into the surface.

License

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Author Information

#	Name	Institute / Affiliation
1	Saddam Hussain	Department of Mechanical Engineering, SOE, SSSUTMS, M.P., INDIA
2	Priyanka Jhawar	Department of Mechanical Engineering, SOE, SSSUTMS, M.P., INDIA
3	Dr. G.R.Selokar	Department of Mechanical Engineering, SOE, SSSUTMS, M.P., INDIA
4	Anil Verma	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, Jhawar, Priyanka, G.R.Selokar, Dr., & Verma, Anil (2019). INVESTIGATION OF BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT. International Journal of Advance Research and Innovative Ideas In Education, 5(4), 1244-1250.

MLA Style

Hussain, Saddam, et al. "INVESTIGATION OF BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT." International Journal of Advance Research and Innovative Ideas In Education, vol. 5, no. 4, 2019, pp. 1244-1250.

IEEE Style

Saddam Hussain, Priyanka Jhawar, Dr. G.R.Selokar, and Anil Verma, "INVESTIGATION OF BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT," International Journal of Advance Research and Innovative Ideas In Education, vol. 5, no. 4, pp. 1244-1250, 2019.

Vancouver Style

Hussain Saddam, Jhawar Priyanka, G.R.Selokar Dr., Verma Anil. INVESTIGATION OF BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT. International Journal of Advance Research and Innovative Ideas In Education. 2019;5(4):1244-1250.

Harvard Style

Hussain, Saddam, Jhawar, Priyanka, G.R.Selokar, Dr., & Verma, Anil (2019) 'INVESTIGATION OF BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT', International Journal of Advance Research and Innovative Ideas In Education, 5(4), pp. 1244-1250.

Chicago Style

Hussain, Saddam, et al. "INVESTIGATION OF BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT." International Journal of Advance Research and Innovative Ideas In Education 5, no. 4 (2019): 1244-1250.

Turabian Style

Hussain, Saddam, et al. "INVESTIGATION OF BALISTIC MISSILE FIN CONFIGURATION DURING SUPERSONIC FLIGHT." International Journal of Advance Research and Innovative Ideas In Education 5, no. 4 (2019): 1244-1250.