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Search Results for “ai”

6,014 results · showing 2381–2400 · 350 ms

Search Results

  1. PDF

    840_Tuesday_Ilcewicz

    …1) Work with industry, other government agencies, and academia to ensure safe and efficient deployment of composite technologies used in existing and future aircraft 2) Update policies, advisory circulars, training, and detailed background used to support standardized composite practices * Efforts started in 1999 to address issues associated with…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/840_Tuesday_Ilcewicz.pdf

  2. PDF

    5915-01-Exp-08-31-2026

    SCOPE OF ACCREDITATION TO ISO/IEC 17025:2017 NATIONAL INSTITUTE FOR AVIATION RESEARCH (NIAR) – ENVIRONMENTAL TEST LAB 3800 S Oliver Wichita, KS 67210 Reid Owens 620-655-5686 email: reid.owens@idp.wichita.edu ELECTRICAL Valid to: August 31, 2026 Certificate Number: 5915.01 In recognition of the successful completion of the A2LA evaluation process,…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/5915-01-Exp-08-31-2026.pdf

  3. PDF

    NMS-380-TC380-Rev-A-October-2-2025

    … Document No.: NMS 380, Revision A, October 2, 2025 NCAMP Material Specification 350F Autoclave Cure, Toughened Epoxy Prepregs Toray TC380 This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 Prepared by: Reviewed by: Vinsensius Tanoto (NCAMP) Russell Kirkman (Toray TAC), Joe Feskanin (Toray TAC),…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-380-TC380-Rev-A-October-2-2025.pdf

  4. PDF

    JAMS2024-FAA-RBT

    … 4 Background • • Evaluation of bond line integrity and durability of adhesively bonded composite rotor blades is imperative to the safe operation. Retired blades from aged aircraft are will be • • • • Thoroughly Inspected with numerous NDI techniques. Physically tested with high-stress low-cycle loading conditions. Torn apart to perform small scale…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/JAMS2024-FAA-RBT.pdf

  5. PDF

    CACRC-Lamia

    CACRC Depot Bonded Repair Investigation – Round Robin Testing 2013 Technical Review John Tomblin and Lamia Salah National Institute for Aviation Research Wichita State University CACRC Depot Bonded Repair Investigation – Round Robin Testing  Principal Investigators & Researchers -John Tomblin Ph.D., Lamia Salah Ph.D. -Chathuranga Kuruppuarachchige,…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/CACRC-Lamia.pdf

  6. PDF

    NPS_85321_Rev_D_8.12.2025_5320-1_Process_Spec

    NPS 85321 Rev D Date: August 12, 2025 Document No.: NPS 85321, Revision D, August 12, 2025 NCAMP Process Specification This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 Fabrication of NMS 532 Qualification, Equivalency, and Acceptance Test Panels (Solvay (formerly Cytec) Cycom 5320-1) Prepared…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NPS_85321_Rev_D_8.12.2025_5320-1_Process_Spec.pdf

  7. PDF

    W1300_UW_RassainFeraboli

    …of Composite Materials (End of Year II) Presented at the JAMS review meeting Wichita, KS July 21-22, 2009 Prof. Paolo Feraboli University of Washington 1 1 Dr. Mostafa Rassaian Boeing Research & Technology Outline Motivation ƒ Complete lack of standards and accepted practices in testing and analysis of composites under crash conditions Benefits to …

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/W1300_UW_RassainFeraboli.pdf

  8. PDF

    NMS-755-Rev-B_Carbon-Fiber-FR-A_11-13-23

    NMS 755 Rev B Date: November 13, 2023 Document No.: NMS 755, Revision B, November 13, 2023 NCAMP Material Specification This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 Filament Specification (Carbon Fiber FR-A™) (Markforged - MFD) Prepared by: John Tomblin (NCAMP/NIAR), Neville Tay…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-755-Rev-B_Carbon-Fiber-FR-A_11-13-23.pdf

  9. PDF

    CACRCDepotBondedLSalah

    CACRC Depot Bonded Repair Round Robin Investigation Presented by: Lamia Salah March 31st, 2015 JAMS 2015 Technical Review CACRC Depot Bonded Repair Investigation  Principal Investigators & Researchers    John Tomblin Ph.D., Lamia Salah Ph.D. Chathuranga Kuruppuarachchige, Ruchira Walimunige FAA Technical Monitors Curtis Davies, Lynn Pham Other FAA…

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

  10. PDF

    1245_Tuesday_Salah

    Effects of Several Variables on the performance of Repairs Applied to Laminate and Sandwich Structures July 10th, 2007 The Joint Advanced Materials and Structures Center of Excellence Research Team ¾ Principal Investigators & Researchers – – – – – Dr. John Tomblin, Wichita State University Lamia Salah, Wichita State University Dr. Charles Yang, Wichita…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/1245_Tuesday_Salah.pdf

  11. PDF

    Renegade-8HS-Quartz-fabric-CAM-RP-2024-007-Rev-A-10.8.25-MPDR

    …032302 NCAMP Test Report Number: CAM-RP-2024-007 Rev A Report Date: October 8, 2025 Testing Facility: National Institute for Aviation Research Wichita State University 1845 N. Fairmount Wichita, KS 67260-0093 Renegade Materials Corporation 3363 South Tech Blvd Miamisburg, OH 45342 Test Panel Fabrication Facilities: Resonant Sciences 4085 Executive Dr.…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/Renegade-8HS-Quartz-fabric-CAM-RP-2024-007-Rev-A-10.8.25-MPDR.pdf

  12. PDF

    TorayTC1225UnitapeNCP-RP-2019-011RevA5.14.2021SARFinal

    …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: Toray (Former TenCate) v.d. Muelenweg 2 7443 RE Nijverdal Netherlands Distribution Statement A. Approved for public…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/TorayTC1225UnitapeNCP-RP-2019-011RevA5.14.2021SARFinal.pdf

  13. PDF

    Comparison-of-Viscoelastic-Viscoplastic-Models-Chen

    …in bonded joints • High shear load • Behave differently from adhesive bulks • Edge effect, higher shear near edge • Reliable strain measurement method • Strain response to cyclic loads • Ratcheting • Time-dependent, Plastic • Material damage & fatigue life • Constitutive model • Viscoelasticity, Viscoplasticity • Damage Lloyd Smith/Yi Chen- WSU JAMS…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/Comparison-of-Viscoelastic-Viscoplastic-Models-Chen.pdf

  14. PDF

    Effects_of_Defects_in_Composite_Materials_at_Elevated_Strain_Rates-bhasin

    Effects of Defects in Composite Materials at Elevated Strain Rates Federal Aviation Administration Presented by: Akhil Bhasin NIAR-AVET Joint Centers of Excellence for Advanced Materials JAMS Technical Review April 20, 2023 Agenda • • • • Research Team Project Motivation Project Breakdown and Approach Task II – – – • • • • Laminate Fabrication…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/Effects_of_Defects_in_Composite_Materials_at_Elevated_Strain_Rates-bhasin.pdf

  15. PDF

    800_Thursday_Raju

    …Bakuckas • FAA Technical Monitor – Curtis Davis • Other FAA Personnel Involved – F. Leone (Drexel Co-op) • Industry Participation – – – – – Adam Aircraft Co.( P. Harter, B. Allbritten) Toray Composites ( L. Cook) NSE Composites ( T. Walker) Hostert Technical Services ( R. Hostert) Peter Rohl ( Advatech Pacific) The Joint Advanced Materials and…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/800_Thursday_Raju.pdf

  16. 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

  17. PDF

    Toray-TC1225-LM-PAEK-T700GC-UNI-Qualification-CAM-RP-2025-016-RevA-2.24.2026-MPDR-Final

    …NCAMP Test Report Number: CAM-RP-2025-016 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-CAM-RP-2025-016-RevA-2.24.2026-MPDR-Final.pdf

  18. PDF

    NCP-RP-2023-005-Rev-NC-HexPEKK-Statistical-Analysis-Report

    …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 Fabrication Facility: Hexcel Corporation 250 Nutmeg Rd S. South Windsor, CT 06074 1 Distribution Statement A. Approved for public release;…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/NCP-RP-2023-005-Rev-NC-HexPEKK-Statistical-Analysis-Report.pdf

  19. PDF

    Resin-Infused-Fiber-Reinforced-Materials-Guidelines-andrulonis

    Resin Infused Fiber Reinforced Materials Guidelines for Aircraft Design and Certification Process »April 2023 UPDATE Presented by: John Tomblin Rachael Andrulonis Michelle Man Royal Lovingfoss April 19, 2023 Introduction • Resin Infused Fiber Reinforced Materials Guidelines for Aircraft Design and Certification Process • Project Participants • Dr. John…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/Resin-Infused-Fiber-Reinforced-Materials-Guidelines-andrulonis.pdf

  20. PDF

    FAA_JAMS_TEARDOWN_07

    …of Excellence Background ¾ The starship program was officially launched in 1982. ¾ Objectives were to produce the most advanced turboprop business airplane feasible at the time and to promote the use of composites in a business aircraft ¾ Benefits: to achieve elaborate contours through composite molding, lower part count, manufacturing simplicity,…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/FAA_JAMS_TEARDOWN_07.pdf

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