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FAA Technical Library

Technical reports, Tech Notes, and articles that document the FAA’s applied research, engineering, testing and evaluation, and resulting scientific solutions addressing current and future air transportation challenges in collaboration with industry, academia, and other government partners. For more content, visit the FAA Technical Library https://www.faa.gov/about/office_org/headquarters_offices/ang/library/. Bookmark this collection:https://rosap.ntl.bts.gov/collection_faa_tl or https://doi.org/10.21949/1530830.

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United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center 2

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Experimental Testing to Characterize Plastic Deformation, Dynamic Response, and Ductile Fracture of Inconel 718 Under Various Loading Conditions

CITE Title : Experimental Testing to Characterize Plastic Deformation, Dynamic Response, and Ductile Fracture of Inconel 718 Under Various Loading Conditions Creator(s) : Ressa, Aaron;Liutkus, Timothy;Seidt, Jeremy;Gilat, Amos;Cordasco, Daniel; Corporate Creator(s) : Ohio State University. Dynamic Mechanics of Materials Laboratory (DMML);United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center; Corporate Contributor(s) : United States. Federal Aviation Administration. Aircraft Certification Service Policy and Innovation Division Published Date : 2023-09-01 Report Number : DOT/FAA/TC-23/52 DOI : https://doi.org/10.21949/1528240 "Experimental Testing to Characterize" (2023). https://doi.org/10.21949/1528240 "Experimental Testing to Characterize Plastic Deformation, Dynamic Response, and Ductile Fracture of Inconel 718 Under Various Loading Conditions" (2023), https://doi.org/10.21949/1528240 "Experimental Testing to Characterize Plastic Deformation, Dynamic Response, and Ductile Fracture of Inconel 718 Under Various Loading Conditions" , 2023, https://doi.org/10.21949/1528240 Export RIS Citation Information.

:

Ressa, Aaron ;

Liutkus, Timothy

2023-09-01

:

A team consisting of Federal Aviation Administration (FAA) Propulsion Research Program, The Ohio State University (OSU), George Mason University (GMU)...
Aluminum 2024-T351 Input Parameters for *MAT_224 in LSDYNA, Part 2: Additional Tests to Determine Plastic Heating and Ductile Fracture Behavior Under Combined Loading

CITE Title : Aluminum 2024-T351 Input Parameters for *MAT_224 in LSDYNA, Part 2: Additional Tests to Determine Plastic Heating and Ductile Fracture Behavior Under Combined Loading Creator(s) : Seidt, J D;Smith, J. L.;Spulak, N;Lowe, R L;Gilat, A; Corporate Creator(s) : Ohio State University. Dynamic Mechanics of Materials Laboratory (DMML) Corporate Contributor(s) : United States. Department of Transportation. Federal Aviation Administration. Office of Aviation Research and Development Published Date : 2022-08-01 Report Number : DOT/FAA/TC-19/41, P2 DOI : https://doi.org/10.21949/1524500 "Aluminum 2024-T351 Input Parameters" (2022). https://doi.org/10.21949/1524500 "Aluminum 2024-T351 Input Parameters for *MAT_224 in LSDYNA, Part 2: Additional Tests to Determine Plastic Heating and Ductile Fracture Behavior Under Combined Loading" (2022), https://doi.org/10.21949/1524500 "Aluminum 2024-T351 Input Parameters for *MAT_224 in LSDYNA, Part 2: Additional Tests to Determine Plastic Heating and Ductile Fracture Behavior Under Combined Loading" , 2022, https://doi.org/10.21949/1524500 Export RIS Citation Information.

:

Seidt, J D ;

Smith, J. L.

2022-08-01

:

A team consisting of The Ohio State University (OSU), George Mason University (GMU), National Aeronautics and Space Administration Glenn Research Cent...