Investigation of The Effects of Material Change in Aircraft Horizontal Stabilizer Honeycomb Sandwich Panel (HSP) Based on Sandwich Structure Standard Assessment Test Simulation

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S. Solgi; JAHANGIRI A.; Nallaei M.

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Journal: JOURNAL OF MECHANICAL ENGINEERING Year:2018 | Volume:48 | Issue:3 (84) Page(s): 143-151

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Title

Investigation of The Effects of Material Change in Aircraft Horizontal Stabilizer Honeycomb Sandwich Panel (HSP) Based on Sandwich Structure Standard Assessment Test Simulation

Author(s)

S. Solgi | JAHANGIRI A. | Nallaei M. | Issue Writer Certificate

Keywords

Metal Sandwich panels

Von-Mises criterion-Nickel super alloy

Stainless steel

Abstract

Sandwich panel structures because of desirable properties such as high strength to mass ratio and damping of impact energy, have wide application in aero structures. In this article 7 alloys including Stainless steel 321, Stainless steel 347, Inconel 625, Inconel 718, Inconel 600 and nickel alloy 201 have been selected based on similar studies for replacing original part in aircraft horizontal tail. Yield load and damaged area determined by von-mises damage criteria based on methods in MIL-STD-401. Finally two alloys out of these seven alloys passed six parameters consist of damage onset, mechanical properties on 650 OC, density, price and environmental effects have been nominated. Results illustrated that Inconel 625 and Inconel 718 are best candidates for replacing current material of horizontal tail structure.

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APA: Copy

S., Solgi, JAHANGIRI, A., & Nallaei, M.. (2018). Investigation of The Effects of Material Change in Aircraft Horizontal Stabilizer Honeycomb Sandwich Panel (HSP) Based on Sandwich Structure Standard Assessment Test Simulation. JOURNAL OF MECHANICAL ENGINEERING, 48(3 (84) ), 143-151. SID. https://sid.ir/paper/270142/en

Vancouver: Copy

S. Solgi, JAHANGIRI A., Nallaei M.. Investigation of The Effects of Material Change in Aircraft Horizontal Stabilizer Honeycomb Sandwich Panel (HSP) Based on Sandwich Structure Standard Assessment Test Simulation. JOURNAL OF MECHANICAL ENGINEERING[Internet]. 2018;48(3 (84) ):143-151. Available from: https://sid.ir/paper/270142/en

IEEE: Copy

Solgi S., A. JAHANGIRI, and M. Nallaei, “Investigation of The Effects of Material Change in Aircraft Horizontal Stabilizer Honeycomb Sandwich Panel (HSP) Based on Sandwich Structure Standard Assessment Test Simulation,” JOURNAL OF MECHANICAL ENGINEERING, vol. 48, no. 3 (84) , pp. 143–151, 2018, [Online]. Available: https://sid.ir/paper/270142/en

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