Numerical Simulation of Supersonic Aircraft Surface Aerodynamic Heating and Infrared Radiation Characteristics

Pei Ran Su; Qi Tai Eri; Xi Xi Li

doi:10.4028/www.scientific.net/AMM.444-445.1234

Paper Titles

Numerical Simulation of the Dynamics of Heart Valves: A Literature Review
p.1211

Balance Adjustment of the Gravel-Sand River Downstream Reservoir
p.1218

Numerical Simulation on the Temperature Field of Steel 1045 Quenched by Different Hardening Media
p.1222

A Case Study of Application of Modern Design of Experiment Methods in High Speed Wind Tunnel Test
p.1229

Numerical Simulation of Supersonic Aircraft Surface Aerodynamic Heating and Infrared Radiation Characteristics
p.1234

Remote Sensing Integration Survey of Typical Land Types and Analysis of its Spectral Properties in Southeast of Yunnan Province
p.1239

Study on Remote Sensing Image Auto-Identify Classification by Used of Object-Oriented Technology
p.1244

Mechanical Numerical Analysis for L-Shape Traffic Signs Bar with Variable Cross-Section
p.1250

The Urban Space Expansion Analysis in Mountain Areas Based on GIS and RS
p.1255

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 444-445Numerical Simulation of Supersonic Aircraft...

Numerical Simulation of Supersonic Aircraft Surface Aerodynamic Heating and Infrared Radiation Characteristics

Abstract:

The aerodynamic heating and infrared radiation characteristics of BrahMos supersonic cruise missile were investigated. The aerodynamic heating was simulated using finite volume method, and the infrared radiation characteristics were simulated by reverse Monte Carlo method. Infrared radiation characteristics of missile surface were analyzed in different surface emissivity and flight altitudes, and the effects of environmental radiation and atmospheric attenuation were considered. The results show 8~14μm and 3~5μm environment radiation were approximately 10% and 2.4% of total radiation respectively, when the surface emissivity is 0.3. The proportion of environmental radiation reduces nearly half when the surface emissivity increases by 0.2.

You might also be interested in these eBooks

Advances in Computational Modeling and Simulation

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 444-445)

Pages:

1234-1238

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.444-445.1234

Citation:

Cite this paper

Online since:

October 2013

Authors:

Pei Ran Su, Qi Tai Eri, Xi Xi Li

Keywords:

Aerodynamic Heating, Infrared Radiation, Reverse Monte Carlo, Supersonic Aircraft

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Shripad P. Mahulikar, Hemant R. Sonawane, G. Arvind Rao. Infrared signature studies of aerospace vehicles. Progress in Aerospace Sciences. 43 (2007), 218–245.

DOI: 10.1016/j.paerosci.2007.06.002

Google Scholar

[2] SHAN Yong, ZHANG Jingzhou, GUO Rongwei. Numerical computation and analysis of the infrared radiation characteristic of missile scarf skin. Journal of Aerospace Power. 23 (2008), 251-255.

Google Scholar

[3] LV Jianwei, WANG Qiang. Numerical calculation and analysis of infrared radiation characteristics from aircraft skin by using RMC method. INFRARED AND LASER ENGINEERING. 38(2009) 232-237.

Google Scholar

[4] Michael F. Modest. Radiative Heat Transfer. 2nd Edition. San Diego: Academic Press, (2003).

Google Scholar

[5] L. H. Liu. Backward Monte Carlo Method Based on Radiation Distribution Factor. J. THERMOPHYSICS. 18 (2003) 151-153.

Google Scholar

[6] M. Matsumoto and T. Nishimura. A 623 Dimensionally Equidistributed Uniform Pseudo Random Number Generator. ACM Transactions on Modeling and Computer Simulation, 8 (1998) 3-30.

DOI: 10.1145/272991.272995

Google Scholar

[7] Donald Hearn, M. Pauline Baker. Computer Graphics with OpenGL Third Edition. Prentice Hall, (2003).

Google Scholar