Analysis on Steady Temperature of Honeycomb-Core Panel Based on Coupled Aerothermal Heating and Honeycomb Conduction

Wei Liang; Yu Fu; Zhen Qi Liu; Lu Lu Yang; Han Chao Mai

doi:10.4028/www.scientific.net/AMR.217-218.1197

Paper Titles

Effect of Refining Slag on the Inclusions of Hard Wire Steel during Melting Process
p.1174

Influence of Cold Working and Grain Size on Pitting Corrosion Resistance of Ferritic Stainless Steel
p.1180

Simulation and Calculation to Segregation of High Nitrogen Steels Solidification Process Based on PROCAST Software
p.1185

The Effect of Pressure and Pore-Forming Agent on the Mechanical Properties of Porous Titanium
p.1191

Analysis on Steady Temperature of Honeycomb-Core Panel Based on Coupled Aerothermal Heating and Honeycomb Conduction
p.1197

Characterization and Possibility of Coconut Filter Fibers as Reinforcement for Polymers
p.1202

Study on the Compression Properties of Epoxy Matrix Composites Reinforced by PES Warp-Knitted Spacer Fabric
p.1208

Controlled Hydrothermal Synthesis of ZnO Nano and Microstructure Materials with Photocatalytic Properties
p.1212

OWL-Based Description for Agent
p.1218

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 217-218Analysis on Steady Temperature of Honeycomb-Core...

Analysis on Steady Temperature of Honeycomb-Core Panel Based on Coupled Aerothermal Heating and Honeycomb Conduction

Abstract:

A physical model is formulated to evaluate the steady temperature field of honeycomb-core panel. The model takes into account the coupled effect of aerothermal heating and radiate energy from front and rear plate and honeycomb thermal conduction. The equations that are established based on the model are solved in numerical method and the equivalent thermal conductivity is obtained. The model is also used to investigate the effect of coming fluid and the geometric parameters of honeycomb structure on the TPS capacity.

You might also be interested in these eBooks

High Performance Structures and Materials Engineering

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 217-218)

Pages:

1197-1201

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.217-218.1197

Citation:

Cite this paper

Online since:

March 2011

Authors:

Wei Liang, Yu Fu, Zhen Qi Liu, Lu Lu Yang, Han Chao Mai

Keywords:

Grey Body, Honeycomb-Core Panel, MTPS, Temperature Field

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] L. Yi, Y. Peng, Q. Sun. Research of the Higher-order Finite Element Arithmetic for Radiation Exchange. Chinese Journal of Aeronautics. 9(3): 197-202, (2006).

DOI: 10.1016/s1000-9361(11)60345-2

Google Scholar

[2] N.D. Kaushika, R. Padmapriya, T.P. Singh. Convection Theory of Honeycomb and Slat Devices for Solar Energy Applications. Energy Res Technol, 1992, 35(2): 126-146.

Google Scholar

[3] Riley C.J. An engineering aerodynamic heating method for hypersonic flow. AIAA, NASA Langley Research Center (1992).

Google Scholar

[4] Cummings, Mary L. A Compute Code (Skintemp) For Predicting Transient Missile and Aircraft Heat Transfer Characteristics [R]. Naval Postgraduate School, Monterey, (1994).

Google Scholar

[5] S. Yang, W. Tao. Heat Transfer. Higher Education Press. (1998) p: 240-241.

Google Scholar

[6] S. A. Bouslog, B. Moore, I. Lawson. X-33 Metallic TPS Tests in NASA-LaRC High Temperature Tunnel, AIAA, NASA Langley Research Center, (1999).

DOI: 10.2514/6.1999-1045

Google Scholar