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HybridCert-WSeneviratne

Fatigue and Residual Strength Analysis of Composite Material Damage Tolerance Testing and Analysis Protocols for Full-Scale Composite Airframe Structures under Repeated Loading 2015 Technical Review Waruna Seneviratne Wichita State University/NIAR Certification of Composite-Metal Hybrid Structures • Motivation and Key Issues – Damage growth mechanics,…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/HybridCert-WSeneviratne.pdf

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W1220_WSU_Olivares

…Research Program Overview Phase I: HII and HIII FAA Numerical ATD Validation [ July 2005 - July 2009]: – Test variability HII and HIII FAA ATD with 2,3, and 4point restraints. – Numerical ATD V&V Procedure. – Comparison HII and HIII FAA Dynamic Performance. – SAE ARP ATD Reference Data. Phase II: Seat Structural Modeling Techniques [ September 2006 …

https://www.wichita.edu/industry_and_defense/NIAR/Documents/W1220_WSU_Olivares.pdf

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NMS-219-Rev-B-August-21-2024-EP2190-Base-Material-Spec

NMS 219 Rev B Date: August 21, 2025 Document No.: NMS 219, Revision B, August 21, 2025 NCAMP Material Specification This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 350F Autoclave Cure, High Toughness Epoxy Prepregs Syensqo EP2190 Prepared by: Evelyn Lian (NCAMP/NIAR), Vinsensius Tanoto…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-219-Rev-B-August-21-2024-EP2190-Base-Material-Spec.pdf

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Toray-TC380-T1100GC-24K-Uni-NCP-RP-2025-010-Rev-10-03-25-SAR

…Institute for Aviation Research Wichita State University Wichita, KS 67260 Testing Facility: National Institute for Aviation Research Wichita State University 1845 N. Fairmount Wichita, KS 67260 Test Panel Fabrication Facility: National Center for Aviation Training (NCAT) Wichita State University Tech 4004 North Webb Rd Wichita, KS 67226…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/Toray-TC380-T1100GC-24K-Uni-NCP-RP-2025-010-Rev-10-03-25-SAR.pdf

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Toray-TC1225-LM-PAEK-T700GC-UNI-Qualification-NCP-RP-2025-008-RevA-2-24-2026-SAR-Final

…NCAMP Report Number: NCP-RP-2025-008 Rev A Report Date: February 24, 2026 Testing Facility: National Institute for Aviation Research (NIAR) Wichita State University 1845 N. Fairmount Wichita, KS 67260-0093 Test Panel Fabrication Facility: Advanced Technologies Lab for Aerospace Systems (ATLAS) National Institute for Aviation Research (NIAR) Wichita…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/Toray-TC1225-LM-PAEK-T700GC-UNI-Qualification-NCP-RP-2025-008-RevA-2-24-2026-SAR-Final.pdf

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W0820_UW_Livne

The Effects of Damage and Uncertainty on the Aeroelastic / Aeroservoelastic Behavior and Safety of Composite Aircraft Presented by Professor Eli Livne Department of Aeronautics and Astronautics University of Washington JAMS Meeting, July 2009 1 Contributors • • • • • Department of Aeronautics and Astronautics • Dr. Eli Livne – PI, Professor…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/W0820_UW_Livne.pdf

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CAM-RP-2018-013-NC-Stratasys-Certified-ULTEM-9085-MPDR-Rev-A-12-02-20

… 031701 NCAMP Test Report Number: CAM-RP-2018-013 Rev A Report Date: December 02, 2020 Testing Facility: National Institute for Aviation Research Wichita State University 1845 N. Fairmount Wichita, KS 67260-0093 Test Coupon Fabrication Facility: RP+M 33490 Pin Oak Pkwy Avon Lake, OH 44012 Distribution Statement A. Approved for public release; distribution …

https://www.wichita.edu/industry_and_defense/NIAR/Documents/CAM-RP-2018-013-NC-Stratasys-Certified-ULTEM-9085-MPDR-Rev-A-12-02-20.pdf

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WG4-Working-Group-4-Debrief-Notes

…processes used for AM aviation parts. 1.6 The classification scheme in this practice establishes a consistent methodology to define and communicate the consequence of failure associated with AM aviation parts. 1.7 This practice is not intended to supersede the requirements and definitions of the applicable regulations or policies, including but not…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/WG4-Working-Group-4-Debrief-Notes.pdf

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2024JAMS2024-HLBBT

…B Design Value Development Standardization Opportunity Allowables Development Material, Process, and Configuration Behavior Data TECHNICAL DESCRIPTION A unique test methodology aimed at detecting bonded joints, sandwich designs, attachment features etc. The methodology aims to bridge the gap between coupon & components level test. Primary goal is to…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/2024JAMS2024-HLBBT.pdf

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415-Salviato_Yang_Tuttle-JAMS-2017

Certification of Discontinuous Composite Material Forms for Aircraft Structures Marco Salviato, Seunghyun Ko, Jinkyu Yang, Mark Tuttle University of Washington JAMS 2017 Technical Review March 21, 2017 Research team outline Research team outline • Seunghyun Ko (PhD student); • Reed Hawkins (Master student) Reda El Mamoune (Master student) ZT Yang…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/415-Salviato_Yang_Tuttle-JAMS-2017.pdf

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Impact-damage-tolerance-guidelines-kim

…Aug 2021 June 2025 Ben Katko 2018 Mechanical Engineering, New Mexico Institute of Mining and Technology Sept. 2018 April 2023 Chengyang Huang 2019 Shanghai Jiao Tong Univ. Mechanical Engineering September 2020 March 2024 ▪ MS: none • • • FAA Technical Monitor: Lynn Pham FAA Sponsors: Larry Ilcewicz & Cindy Ashforth Other FAA Personnel…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/Impact-damage-tolerance-guidelines-kim.pdf

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NMS-201-slash-1-Rev-B-2025-10-8

NMS 201/1 Rev B Date: October 8, 2025 Document No.: NMS 201/1 Revision B, October 8, 2025 NCAMP Material Specification This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 Autoclave Cure, Prepreg, Type 38, Class 2, Grade 286, Style 8HS Renegade RM-2014-LDk-Tk Low Dielectric Epoxy Prepreg 4581 8HS…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-201-slash-1-Rev-B-2025-10-8.pdf

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NMS-765-Base-Rev-March-10-2024

…Revision -, March 10, 2025 NCAMP Material Specification Vacuum-Bag-Only or Autoclave Cure Epoxy Prepregs Park Aerospace Corp. E765 Prepregs This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 Prepared by: Reviewed by: Vinsensius Tanoto (NCAMP) Kelly Jacob (Park Aerospace Corp.), Dhivakar Kumar…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-765-Base-Rev-March-10-2024.pdf

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DelaminationDisbondArrestFeaturesinAircraftCompositeStructures-Richard-Lin

Delamination/Disbond Arrest Features in Aircraft Composite Structures Luke Richard and Kuen Y. Lin University of Washington JAMS Technical Review March 31-April 1, 2015 Sponsored Project Information • Principal Investigator: • Dr. Kuen Y. Lin, Aeronautics and Astronautics, UW • Research Assistant: Luke Richard UW • FAA Technical Monitor: Lynn Pham • Other …

https://www.wichita.edu/industry_and_defense/NIAR/Documents/DelaminationDisbondArrestFeaturesinAircraftCompositeStructures-Richard-Lin.pdf

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CAM-RP-2023-007-NC-Additively-Manufactured-Hexpekk-100

…NCAMP Test Report Number: CAM-RP-2023-007 Rev N/C Report Date: January 22nd, 2025 Testing Facility: National Institute for Aviation Research Wichita State University 1845 N. Fairmount Wichita, KS 67260-0093 Test Coupon Fabrication Facility: Hexcel Corporation 250 Nutmeg Rd S. South Windsor, CT 06074 Distribution Statement A. Approved for public…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/CAM-RP-2023-007-NC-Additively-Manufactured-Hexpekk-100.pdf

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Effects-of-Alternative-Jet-Fuel-Blends-kundu

… geometries Approach • • Experimental investigation of conventional and alternative fuels absorption of carbon/epoxy composites • Track the weight gain with time to determine the amount of fuel absorbed • Investigate the changes in the dynamic properties after absorption Modeling the diffusion process using Finite Element Method Literature Study:…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/Effects-of-Alternative-Jet-Fuel-Blends-kundu.pdf

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NCAMP-DRAM-RGB-Bylaws-NCD-110-202505

…5 Section 2. Voting Members ............................................................................................. 5 Section 3. Waiver Procedures .......................................................................................... 5 ARTICLE IV MEETINGS…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/NCAMP-DRAM-RGB-Bylaws-NCD-110-202505.pdf

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AircraftSkinProtectionEffectivenessRevA

Page i Aircraft Skin Protection Effectiveness Report No 22-2152-RR52865, Rev A Lightning Direct Effects Handbook Revision Letter Initial Release Date Released 11/03/2022 Report Number 22-51512RTR52865 Author Rebeka Khajehpour & Alyssa Gonzalez Additional Notes NIAR KART R52865 Spliced Lightning Strike Protection on Thermoplastic Composites Page ii…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/AircraftSkinProtectionEffectivenessRevA.pdf

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Toray-3960-T1100G-Stat-Analysis-Report-NCP-RP-2023-002-RevB-1.5.2026

…Institute for Aviation Research Wichita State University Wichita, KS 67260-0093 Testing Facility: National Institute for Aviation Research Wichita State University 1845 N. Fairmount Wichita, KS 67260-0093 Test Panel Fabrication Facility: Advanced Technologies Lab for Aerospace Systems (ATLAS) National Institute for Aviation Research Wichita State…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/Toray-3960-T1100G-Stat-Analysis-Report-NCP-RP-2023-002-RevB-1.5.2026.pdf

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FailureofNotchedLaminatesUnderOut-of-PlaneBending-Daniels-Parmigiani

Failure of Notched Laminates Under Out-ofPlane Bending, Phase VIII Spring 2015 Mitchell Daniels, Levi Suryan, & John P. Parmigiani Oregon State University Motivation, Objective, and Approach • Motivation and Key Issues Develop analysis techniques useful in design of composite aircraft structures under out-of-plane loading (bending and shear) • Objective…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/FailureofNotchedLaminatesUnderOut-of-PlaneBending-Daniels-Parmigiani.pdf