Heat-transfer has been performed on a sandwich thermal protection system (TPS) for future flight vehicles. The sandwich structures are built from thin walled metal sheets. These structures as a part of the airframe outer cover provide thermal protection to the interior parts mounted inside the vehicle. The temperature protection materials used for sandwich structures should have high strength even at the elevated temperatures. It is easier to simulate the 1500 C (after 1500 C material properties are changed) temperature on the Aluminium sandwich structures and find the temperature gradient across the sandwich depth. Though the experiment was done on hexagonal cells honeycomb, the ANSYS analyses have been done for both square cell’s sandwich panel and hexagonal honeycomb panel for comparison. Experiments are done on using Al alloy honeycomb sandwich panels and the validations of experimental work using ANSYS analysis have been performed. ANSYS modeling, analysis has been done for both, the square and hexagonal honeycomb sandwich panels of the Al alloy. This paper focuses on the heat transfer analysis and in exploring the ways to reduce the heat transfer effect with the methods mentioned above, which could be effectively used for flight vehicle applications
the Static Analysis of Sandwich Panels with Square
Honeycomb Core by the American Institute of
Aeronautics and Astronautics, May 2006 [12]
Investigation on the square cell honeycomb structures
under axial loading, Sen Liang *, H.L. Chen,
Composite Structures 72 (2006) 446–454 [13]
Research progress on thermal protection materials and
structures of hypersonic vehicles, YANG Ya-zheng,
YANG Jia-ling,FANG Dai-ning, Appl. Math. Mech.
Engl. Ed., 2008, 29(1):51–60 [14]
Improved lumped models for transient combined
convective and radiative cooling of multi-layer
composite slabs Chen An, Jian Su Applied Thermal
Engineering 31 (2011) 2508e2517 [15]
MDA of Hexagonal Honeycomb Plates used for Space
Applications, A.Boudjemai , M.H. Bouanane,
Mankour, R. Amri, H. Salem, B. Chouchaoui, World
Academy of Science, Engineering and Technology 66 2012 [16] TALAT Properties, Characteristics and Alloys,
Aluminium: Physical prepared
by Ron Cobden, Alcan, Banbury [17]
for Convective Thermal Protection Systems Joseph F. Rakow
and Anthony M. Waas, Journal Of Spacecraft And Rockets, Vol. 42, No. 5, September–October 2005 [18] On the Static Analysis of Sandwich Panels with Square Honeycomb Core, Hazem E. Soliman*, Dhaval P. Makhecha, Summit Vasudeva, Kapania AIAA/ASME/ASCE/AHS/ASC Structural Dynamics, and Materials Con. 1-4 May 2006, Newport, Rhode Island Rakesh K. and Owen Hughes, 47th Structures,
Heat Insulation Analysis of an Aluminum Honeycomb Sandwich Structure
Year 2015,
Volume: 1 Issue: 3, 210 - 220, 01.03.2015
the Static Analysis of Sandwich Panels with Square
Honeycomb Core by the American Institute of
Aeronautics and Astronautics, May 2006 [12]
Investigation on the square cell honeycomb structures
under axial loading, Sen Liang *, H.L. Chen,
Composite Structures 72 (2006) 446–454 [13]
Research progress on thermal protection materials and
structures of hypersonic vehicles, YANG Ya-zheng,
YANG Jia-ling,FANG Dai-ning, Appl. Math. Mech.
Engl. Ed., 2008, 29(1):51–60 [14]
Improved lumped models for transient combined
convective and radiative cooling of multi-layer
composite slabs Chen An, Jian Su Applied Thermal
Engineering 31 (2011) 2508e2517 [15]
MDA of Hexagonal Honeycomb Plates used for Space
Applications, A.Boudjemai , M.H. Bouanane,
Mankour, R. Amri, H. Salem, B. Chouchaoui, World
Academy of Science, Engineering and Technology 66 2012 [16] TALAT Properties, Characteristics and Alloys,
Aluminium: Physical prepared
by Ron Cobden, Alcan, Banbury [17]
for Convective Thermal Protection Systems Joseph F. Rakow
and Anthony M. Waas, Journal Of Spacecraft And Rockets, Vol. 42, No. 5, September–October 2005 [18] On the Static Analysis of Sandwich Panels with Square Honeycomb Core, Hazem E. Soliman*, Dhaval P. Makhecha, Summit Vasudeva, Kapania AIAA/ASME/ASCE/AHS/ASC Structural Dynamics, and Materials Con. 1-4 May 2006, Newport, Rhode Island Rakesh K. and Owen Hughes, 47th Structures,
Konka, K., Rao, J., & Gupta, K. S. A. (2015). Heat Insulation Analysis of an Aluminum Honeycomb Sandwich Structure. Journal of Thermal Engineering, 1(3), 210-220. https://doi.org/10.18186/jte.25885
AMA
Konka K, Rao J, Gupta KSA. Heat Insulation Analysis of an Aluminum Honeycomb Sandwich Structure. Journal of Thermal Engineering. March 2015;1(3):210-220. doi:10.18186/jte.25885
Chicago
Konka, Kantha, Jayathirtha Rao, and Kumar Swamy AVSS Gupta. “Heat Insulation Analysis of an Aluminum Honeycomb Sandwich Structure”. Journal of Thermal Engineering 1, no. 3 (March 2015): 210-20. https://doi.org/10.18186/jte.25885.
EndNote
Konka K, Rao J, Gupta KSA (March 1, 2015) Heat Insulation Analysis of an Aluminum Honeycomb Sandwich Structure. Journal of Thermal Engineering 1 3 210–220.
IEEE
K. Konka, J. Rao, and K. S. A. Gupta, “Heat Insulation Analysis of an Aluminum Honeycomb Sandwich Structure”, Journal of Thermal Engineering, vol. 1, no. 3, pp. 210–220, 2015, doi: 10.18186/jte.25885.
ISNAD
Konka, Kantha et al. “Heat Insulation Analysis of an Aluminum Honeycomb Sandwich Structure”. Journal of Thermal Engineering 1/3 (March 2015), 210-220. https://doi.org/10.18186/jte.25885.
JAMA
Konka K, Rao J, Gupta KSA. Heat Insulation Analysis of an Aluminum Honeycomb Sandwich Structure. Journal of Thermal Engineering. 2015;1:210–220.
MLA
Konka, Kantha et al. “Heat Insulation Analysis of an Aluminum Honeycomb Sandwich Structure”. Journal of Thermal Engineering, vol. 1, no. 3, 2015, pp. 210-2, doi:10.18186/jte.25885.
Vancouver
Konka K, Rao J, Gupta KSA. Heat Insulation Analysis of an Aluminum Honeycomb Sandwich Structure. Journal of Thermal Engineering. 2015;1(3):210-2.