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  1. PDF

    NPS-80530R-Repair-Process-Specification-12-22-2020

    NPS 80530R Rev Date: December 22, 2020 Document No.: NPS 80530R Rev -, December 22, 2020 Process Specification for Composite Bonded Repair Material Test Panels using Solvay 5320-1 Prepreg (Cured using a Composite Repair Console) Prepared by: John Tomblin, Rachael Andrulonis, Jeff Gilchrist, Royal Lovingfoss Reviewed by: Eric Chesmar, Phil Croft, Rusty…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NPS-80530R-Repair-Process-Specification-12-22-2020.pdf

  2. PDF

    NPS-81225AFP-Rev-D-2-24-2026

    …Distribution Statement A. Approved for public release; distribution is unlimited. National Center for Advanced Materials Performance Wichita State University – NIAR 1845 Fairmount Ave., Wichita, KS 67260-0093, USA Page 1 of 30 February 24, 2026 NPS 81225AFP Rev D REVISIONS Rev - By Ethan McDaniel Date Description 5/17/2024 Initial release. …

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NPS-81225AFP-Rev-D-2-24-2026.pdf

  3. PDF

    Toray-3960-Uni-CAM-RP-2024-004-Rev-A-9.4.25-MPDR-DRAFT

    …15 1.5.1 Process Definition ................................................................................. 15 1.5.2 Specimen & Testing Details .................................................................. 17 1.5.2.1 Tabbing ..................................................................................... 17…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/Toray-3960-Uni-CAM-RP-2024-004-Rev-A-9.4.25-MPDR-DRAFT.pdf

  4. PDF

    EP2190-IMS65-UNI-CAM-RP-2022-001-Rev-9.18.2025-MPDR

    …2025 Testing Facility: Fluid SBS Testing Facility: Solvay 1440 N Kraemer Blvd Anaheim, CA 92806 National Institute for Aviation Research Wichita State University 1845 N. Fairmount Wichita, KS 67260 Test Panel Fabrication Facility: Solvay 1440 N Kraemer Blvd Anaheim, CA 92806 Prepreg Manufacture Facility: Solvay Wrexham Industrial Estate Abenbury Way…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/EP2190-IMS65-UNI-CAM-RP-2022-001-Rev-9.18.2025-MPDR.pdf

  5. PDF

    NMS-397-Rev-A-March-3-2025-3960-Base-Material-Spec

    NMS 397 Rev A Date: March 3, 2025 Document No.: NMS 397, Revision A, March 3, 2025 NCAMP Material Specification This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 High Toughness and High Tensile Performance Epoxy Prepregs Toray Composite Materials America, Inc. 3960 Prepared by: Vinsensius Tanoto,…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-397-Rev-A-March-3-2025-3960-Base-Material-Spec.pdf

  6. PDF

    T0840_FAA_Ilcewicz

    …thrust areas • Progress and Plans Larry Ilcewicz CS&TA Federal Aviation Administration July 21, 2009 – 1999 to present – Future milestones – AC 20-107B – Training initiatives • Review of JAMS – Assessment of existing projects – More industry involvement Ongoing FAA Composite Safety and Certification Initiatives • Actively working with industry…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/T0840_FAA_Ilcewicz.pdf

  7. PDF

    900-Richard-JAMS-2017

    “Delamination/Disbond Arrest Features in Aircraft Composite Structures” JAMS Technical Review Luke Richard and Kuen Y. Lin University of Washington March 21, 2017 Sponsored Project Information • Principal Investigator: • Dr. Kuen Y. Lin, Aeronautics and Astronautics, UW • Research Assistant: Luke Richard, UW (lrich1@uw.edu) • FAA Technical Monitor: Lynn…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/900-Richard-JAMS-2017.pdf

  8. PDF

    300-JAMS-2017-In-Service-Repair

    Inspection and Teardown of Aged In-Service Bonded Repairs 2016 Technical Review Waruna Seneviratne, John Tomblin, and Brandon Saathoff Inspection and Teardown of Aged In-Service Bonded Repairs NIAR Research Team Waruna Seneviratne, PhD John Tomblin, PhD Brandon Saathoff FAA Ahmet Oztekin, PhD (Technical Monitor) Larry Ilcewicz, PhD Rusty Jones David…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/300-JAMS-2017-In-Service-Repair.pdf

  9. PDF

    830-JAMS-2017-DT-Life-Prediction-Wearout

    Analytical Fatigue Life Determination based on Residual Strength Degradation of Composites Damage Tolerance Testing and Analysis Protocols for Full-Scale Composite Airframe Structures under Repeated Loading 2017 Technical Review Waruna Seneviratne and John Tomblin Damage Tolerance Testing and Analysis Protocols for Full-Scale Composite Airframe Structures…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/830-JAMS-2017-DT-Life-Prediction-Wearout.pdf

  10. PDF

    345-JAMS-2017-EKD

    …Palliyaguru • FAA Technical Monitor – Zhi-Ming Chen • Other FAA Personnel Involved – Larry Ilcewicz, PhD and David Westlund • Industry Participation – Cirrus Aircraft 2 Environmental Factor Influence on Composite Design and Certification • Motivation and Key Issues Moisture absorption characteristics of composites can be coupled with realistic…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/345-JAMS-2017-EKD.pdf

  11. PDF

    1115-JAMS_2017_Olivares_final_March2017_Rev1

    …Olivares Ph.D., NIAR-WSU JAMS 2017 Technical Review March 21, 2017 Crashworthiness - Certification by Analysis • Motivation and Key Issues – The introduction of composite airframes warrants an assessment to evaluate that their crashworthiness dynamic structural response provides an equivalent or improved level of safety compared to conventional metallic…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/1115-JAMS_2017_Olivares_final_March2017_Rev1.pdf

  12. PDF

    JAMS2019_Engineering-Approach_Combined-Loading

    …Sandwich Structures Subjected to Combined Compression and Pressure Loading • • • Motivation and Key Issues • Thermo-mechanical loads during ground-air-ground (GAG) cycling result in localized mode I stresses that cause further delamination/disbond/core fracture growth. Objective • Develop an engineering approach for damage tolerance analysis of…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/JAMS2019_Engineering-Approach_Combined-Loading.pdf

  13. PDF

    4-Saathoff-Inspection-and-Teardown

    Inspection and Teardown of Aged In-Service Bonded Repairs JAMS 2019 Technical Review – May 23, 2019 Waruna Seneviratne, John Tomblin, and Brandon Saathoff Research Team NIAR Waruna Seneviratne, PhD John Tomblin, PhD Brandon Saathoff FAA Ahmet Oztekin, PhD (Technical Monitor) Larry Ilcewicz, PhD Cindy Ashforth SNL Stephen Neidigk Ray Ely 2…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/4-Saathoff-Inspection-and-Teardown.pdf

  14. PDF

    15-Andrulonis-Advanced-Fiber-Reinforced-Polymer

    Advanced Fiber Reinforced Polymer Materials Guidelines for Aircraft Design Certification Process John Tomblin, Wichita State University Rachael Andrulonis, Wichita State University Royal Lovingfoss, Wichita State University JAMS 2019 Technical Review May 22 - 23, 2019 Advanced Fiber Reinforced Polymer Materials Guidelines for Aircraft Design Certification…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/15-Andrulonis-Advanced-Fiber-Reinforced-Polymer.pdf

  15. PDF

    8-UCSD-JAM8SPresentation-2017-ImpactNDE-v4

    Impact Damage Formation on Composite Aircraft Structures / Non-Destructive Evaluation Methods for Detecting Major Damage in Internal Composite Structural Components Hyonny Kim, Professor, Dept. Structural Engineering University of California San Diego 2017 JAMS Technical Review March 21, 2017 University of Utah, Salt Lake City, UT Impact Damage Formation…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/8-UCSD-JAM8SPresentation-2017-ImpactNDE-v4.pdf

  16. PDF

    200-JAMS-2017-WSU-LVS

    … conference March 21st 2017 PI: Dr. Lloyd V Smith Washington State University Pullman, WA Graduate students: Preetam C Mohapatra Reza Moheimani David Lemme Durability of Bonded Aircraft Structure • Motivation and Key Issues: • • Adhesive bonding is a key path towards reduced weight in aerospace structures. Certification requirements for bonded structures…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/200-JAMS-2017-WSU-LVS.pdf

  17. PDF

    18-Parmigiani-Evaluation-of-Parameters

    … for both matrix tension and compression in Abaqus (often with the same parameters) Damage propagation Final failure Displacement • A linear elastic region culminating in the point of maximum load carrying ability at damage initiation • A linear plastic region beginning at damage initiation, including all damage propagation, and ending with no load…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/18-Parmigiani-Evaluation-of-Parameters.pdf

  18. PDF

    Core-Material-qualification-guidance-for-aircraft-design-and-cert-bsaathoff

    Core Material Qualification Guidance for Aircraft Design and Certification John Tomblin, Rachael Andrulonis, Royal Lovingfoss, Nicole Stahl & Brandon Saathoff April 19th, 2023 Presented by: Brandon L. Saathoff Senior Research Engineer WSU-NIAR JAMS 2023 Technical Review – Seattle, WA Research Team NIAR • • • • • John Tomblin, PhD Rachael Andrulonis Royal…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/Core-Material-qualification-guidance-for-aircraft-design-and-cert-bsaathoff.pdf

  19. PDF

    IndustryFeedback

    …solutions for metal ƒ Presenters – All did an excellent job Perspective ƒ Large Tier 1 supplier to the aviation industry – Largest supplier to Boeing and Airbus ƒ Design, manufacture, test and certify ƒ Growing use of advanced materials – Section 41 on Boeing 787 – Cab and cabin on CH-53 Summary Comments ƒ ƒ Great work on repair and bonding and…

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

  20. PDF

    NPS_81225_Rev_E_July-30-2025

    …specification covers prepreg cutting, layup and consolidation process with a static press. This specification does not contain all the necessary information typically required in a composite process specification for the fabrication of composite structures, such as personnel qualification and layup room requirements. Users should refer to their existing…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NCAMP/NPS_81225_Rev_E_July-30-2025.pdf