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  1. PDF

    TheEffectsofDamageand-Livne

    Project: The Effects of Damage and Uncertainty on the Aeroelastic / Aeroservoelastic Behavior and Safety of Composite Aircraft Presented by Eli Livne Professor Department of Aeronautics and Astronautics University of Washington JAMS Meeting, April 2011 1 An Overview of the Project covering ▪ Aeroelastic probabilistic reliability analysis of composite…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/TheEffectsofDamageand-Livne.pdf

  2. PDF

    JAMS-Intro-SAMPE-05212024-v4

    …Materials (JAMS) Presenters: Ahmet Oztekin Program Manager Aviation Research Division FAA WJH Technical Center Cindy Ashforth Senior Technical Specialist for Advanced Composite Materials Office of Senior Technical Experts FAA Aviation Safety | Aircraft Certification Service Presented at SAMPE JAMS 2024 May 21, 2024 FAA Joint Centers of Excellence…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/JAMS-Intro-SAMPE-05212024-v4.pdf

  3. PDF

    eVTOL_Crashworthiness_Results_and_Findings_50ft-Battery-Drop-Test-gomez

    … Federal Aviation Administration Presented by: Aswini Kona-Ravi NIAR-WSU Joint Centers of Excellence for Advanced Materials JAMS Technical Review April 20, 2023 Agenda • Digital Engineering Design, Construction, Instrumentation, and Design Validation – AVET 50ft Drop Tower • Pre-Test Analysis: Battery Model 50 ft. Drop Test Evaluation • eVTOL Battery 50…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/eVTOL_Crashworthiness_Results_and_Findings_50ft-Battery-Drop-Test-gomez.pdf

  4. PDF

    240919-WG3-DAY-3-FINAL-SLIDES

    EASA / FAA Industry – Regulator AM Event Working Group 3 Developing a 5 Year Plan to Allow EASA / FAA acceptance – Machine Monitoring Dr. Sebastian Rott: MTU Aero Engines Wichita, 17th -19th September 2024 AM Process Owner Fernando Lartategui Atela: ITP Aero Associate Technical Fellow in ALM CONFIDENTIAL EASA/FAA AM EVENT – WG3 INTRODUCTION & SCOPE…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/240919-WG3-DAY-3-FINAL-SLIDES.pdf

  5. PDF

    NMS-128-Rev-D-March-16-2022-Hexcel-8552-Base-Material-Specification

    Document No.: NMS 128, Revision D, March 16th, 2022 NCAMP Material Specification This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 350ºF Autoclave Cure, Low Flow Toughened Epoxy Prepregs (Hexcel 8552 and 8552S) Prepared by: Yeow Ng, John Tomblin Edited by: Michelle Man (NCAMP, NIAR) Reviewed by:…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-128-Rev-D-March-16-2022-Hexcel-8552-Base-Material-Specification.pdf

  6. PDF

    JAMS-ULTEMPostQual-Andrulonis

    W I C H I TA S TAT E U N I V E R S I T Y •N AT I O N AL I N S T I T U T E F O R AV I AT I O N R E S E AR C H ULTEM 9085 Post Qualification Activities Rachael Andrulonis Royal Lovingfoss Neville Tay Federal Aviation Administration May 22, 2024 Joint Centers of Excellence for Advanced Materials FAA JAMS – Polymer AM | Program Overview P-U9085 ULTEM…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/JAMS-ULTEMPostQual-Andrulonis.pdf

  7. PDF

    JMADD_and_JMADX-SAMPE_2025_v2

    N AT I O N A L I N S T I T U T E F O R AV I AT I O N R E S E A R C H Joint Metal Additive Database Definition (JMADD): Baseline Qualification and Expansion Activities May 20, 2025 Federal Aviation Administration Joint Centers of Excellence for Advanced Materials DISTRIBUTION STATEMENT A. Approved for public release: Distribution is unlimited.…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/JMADD_and_JMADX-SAMPE_2025_v2.pdf

  8. PDF

    Meeting-The-Needs-of-the-Aerospace-huberty

    Meeting The Needs of the Aerospace Industry: Accurate Simulation of Fabric Permeability Advanced Composites Institute Home of the Marvin B. Dow Stitched Composites Development Center Mississippi Advanced Composites (MAC) Training Center Wayne Huberty, PhD Associate Director, Advanced Composites Institute FAA Technical Monitor: Dave Stanley / FAA Sponsors: …

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/Meeting-The-Needs-of-the-Aerospace-huberty.pdf

  9. PDF

    T1340_Purdue_Sun

    Damage Tolerance and Durability of Adhesively Bonded Composite Structures Thomas Siegmund School of Mechanical Engineering Purdue University The Joint Advanced Materials and Structures Center of Excellence Project II: Development of Improved Hybrid Joints for Composite Structures C.T. Sun, Professor sun@purdue.edu, School of Aeronautics & Astronautics,…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/T1340_Purdue_Sun.pdf

  10. PDF

    NCAMP-Repair-Equivalence-Report_Laminate-Repair-Prepreg-NCP-RP-2018-017-RevNC-12-19-19-SAR-Final

    …No: NCP-RP-2018-017 Rev N/C Report Date: December 19, 2019 Equivalency Statistical Analysis for Laminate Repair Prepreg Batch of Solvay (Formerly Cytec) 5320-1 T650 3K-PW fabric with 36% RC NCAMP Project Number: NPN 031801 NCAMP Test Report Number: NCP-RP-2018-017 Rev N/C Report Date: December 19, 2019 Elizabeth Clarkson, Ph.D. National Center for Advanced …

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NCAMP-Repair-Equivalence-Report_Laminate-Repair-Prepreg-NCP-RP-2018-017-RevNC-12-19-19-SAR-Final.pdf

  11. PDF

    CMC-ALL-compressed

    CMC Data Review Working Group Meeting CMH-17 1st Joint Coordination Meeting Apr. 25, 2024 Rajiv Naik, University of Connecticut (rajiv.naik@uconn.edu) Matthew Opliger, NIAR (matthew.opliger@idp.wichita.edu) 1 CMC Data Review WG Agenda • Introductions • Vision and Goals • Overview of CMH-17 Data Review process • Overview of CMC Data Review Sections 16-18 in…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/CMC-ALL-compressed.pdf

  12. PDF

    200-JAMS-2017-WSU-LVS

    Durability of bonded aerospace structure JAMS Spring 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…

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

  13. PDF

    NCAMP-289-3-Instruction-Guide-August-18-2022

    Instruction Guide for NCAMP FORM 289-3 August 18, 2022 INSTRUCTION GUIDE FOR NCAMP FORM 289-3 ENGINEERING ACCEPTANCE The purposes of NCAMP FORM 289-3: 1. FORM 289-3 should be submitted by an AER to NCAMP for engineering documentation. 2. Documenting the AER’s feedback of NCAMP documents such as material property report, material specification, process…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NCAMP/NCAMP-289-3-Instruction-Guide-August-18-2022.pdf

  14. PDF

    1045_Wednesday_Lin

    Development of Reliability-Based Damage Tolerant Structural Design Methodology Kuen Y. Lin, Andrey Styuart, Eric Cheung Department of Aeronautics and Astronautics University of Washington July 11, 2007 The Joint Advanced Materials and Structures Center of Excellence Contributors ƒ Principal Investigator: ƒ Dr. Kuen Y. Lin, Aeronautics and Astronautics,…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/1045_Wednesday_Lin.pdf

  15. PDF

    1-Oztekin-Open-Remarks

    …JAMS Tech Review Meeting Charlotte, NC 2 FAA Research Process FAA’s Advanced Materials Research Program & Requirements • Program Scope: • Advanced composite materials and structures including hybrid assemblies used in civil aviation • Current scope also include additive manufacturing • Research Requirements: Three years in advance, FAA proposes…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/1-Oztekin-Open-Remarks.pdf

  16. PDF

    18-Parmigiani-Evaluation-of-Parameters

    … for carbon fiber laminates is computationally efficient but is physically unrealistic and does not correspond to actual material behavior. •Objective • Determine the conditions under which the use of this unrealistic material model causes significant errors in predictions of carbon fiber laminate response to load and load-carrying ability. •Approach •…

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

  17. 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

  18. PDF

    11-Lanza-di-Scalea-Standardization-of-Incandescent-Ignition

    Non-destructive Evaluation Methods for Detecting Major Damage in Internal Composite Structures New Project Title: Impact Damage Tolerance Guidelines for Stiffened Composite Panels Francesco Lanza di Scalea Professor, Dept. of Structural Engineering University of California San Diego 2019 JAMS Technical Review May 22-23, 2019 Charlotte Convention Center, NC …

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/11-Lanza-di-Scalea-Standardization-of-Incandescent-Ignition.pdf

  19. PDF

    19-Kim-Impact-Damage-Formation

    Impact Damage Formation on Composite Aircraft Structures Hyonny Kim, Professor, Dept. Structural Engineering University of California San Diego JAMS 2019 Technical Review May 22-23, 2019 Charlotte, NC Impact Damage Formation on Composite Aircraft Structures • Principal Investigators & Researchers – PI: Prof. Hyonny Kim, Professor, UC San Diego – Graduate…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/jams-presentations/19-Kim-Impact-Damage-Formation.pdf

  20. PDF

    NMS_241_slash-3-Rev-A-UD-Woven-DRWF-10.20.2025

    …Date: October 20, 2025 Document No.: NMS 241/3 Revision A, October 20, 2025 NCAMP Material Acceptance Specification This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 Oven Cure of VARTM Processed Dry Reinforcements with Toughened Epoxy Resin Class 2, Style UD, Grade 190, Level 57 (Tenax™ UD Woven…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NCAMP/NMS_241_slash-3-Rev-A-UD-Woven-DRWF-10.20.2025.pdf