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  1. PDF

    2627ParentTaxableGrantReviewPARRVW

    …INSTRUCTIONS >>> On your students’ 2026-2027 FAFSA you (and your spouse, if applicable) reported taxable college grants, scholarships, or AmeriCorps benefits that were reported to the IRS as income. Most individuals either do not have these taxable items or you may have reported the amount incorrectly on the FAFSA. To ensure the…

    https://www.wichita.edu/administration/financial_aid/documents/2627ParentTaxableGrantReviewPARRVW.pdf

  2. PDF

    Personal_International_Travel_Request_Form

    Personal International Travel Request Form * Indicates a required field SECTION A: TRAVELER INFORMATION Last Name * First Name * myWSU ID * Title (if applicable) Dept/Unit (if applicable) Supervisor (if applicable) SECTION B: GENERAL TRAVEL INFORMATION Dates of Travel: * List all countries you will visit. * Countries you will visit: Describe your…

    https://www.wichita.edu/admissions/international/documents/Personal_International_Travel_Request_Form.pdf

  3. PDF

    International_Travel_Authorization_Form

    * Indicates a required field WSU-Sponsored International Travel Request Form SECTION A: TRAVELER INFORMATION Last Name * First Name * Middle Name myWSU ID * Title (if applicable) Dept/Unit (if applicable) Supervisor (if applicable) SECTION B: GENERAL TRAVEL INFORMATION Purpose of Trip: * Conference or Presentation Research Student Recruitment…

    https://www.wichita.edu/admissions/international/documents/International_Travel_Authorization_Form.pdf

  4. PDF

    NCP-RP-2008-008-Rev-NC-IM7-M-cure-Equivalence-Report-3-21-19

    Report No: NCP-RP-2008-008 Rev N/C Report Date: March 21, 2019 Solvay (Formerly Advanced Composites Group) MTM45-1/IM7-145-32%RW (12K IM7 UNI) M cure cycle compared to MH cure cycle Equivalency Statistical Analysis Report FAA Special Project Number: SP3505WI-Q NCAMP Document: NCP-RP-2008-008 N/C Report Date: March 21, 2019 Elizabeth Clarkson, Ph.D. National…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/cytec-mtm45-1/NCP-RP-2008-008-Rev-NC-IM7-M-cure-Equivalence-Report-3-21-19.pdf

  5. PDF

    NCP-RP-2010-010-Rev-NC-MTM45-1-3K-PW-G30-500-LH-Cure

    Report No: NCP-RP-2010-010 Rev N/C Report Date: June 22, 2018 Solvay (Formerly Advanced Composites Group) – MTM45-1 CF0526A-36% RW 3K Plain Weave G30-500 Fabric, 193 gsm Equivalency Statistical Analysis Report – LH Cure Cycle FAA Special Project Number: SP3505WI-Q NCAMP Document: NCP-RP-2010-010 N/C Report Date: June 22, 2018 Elizabeth Clarkson, Ph.D.…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/cytec-mtm45-1/NCP-RP-2010-010-Rev-NC-MTM45-1-3K-PW-G30-500-LH-Cure.pdf

  6. PDF

    CAM-RP-2010-003-NC-Final-Report-ACG_Equivalency_Fabric_LH-M-Cure-Cycle-Rev-A

    NATIONAL INSTITUTE FOR AVIATION RESEARCH Wichita State University CAM-RP-2010-003 N/C, March 9, 2011 Revision A Advanced Composites Group MTM45-1 CF0526A-36%RW 3K Plain Weave G30-500 Fabric, 193 gsm Equivalency Material Property Data Report ACG LH and M Cure Cycle FAA Special Project Number SP3505WI-Q Test Report Number: CAM-RP-2010-003 N/C March 9, 2011…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/cytec-mtm45-1/CAM-RP-2010-003-NC-Final-Report-ACG_Equivalency_Fabric_LH-M-Cure-Cycle-Rev-A.pdf

  7. PDF

    MTM45-1-Material-Model-Development

    …Development Final Project Wrap-Up Prepared by: A. Shahkarami and D. Van Ee Reviewed by: D. Van Ee Approved: A.Poursartip Date: November 15th, 2009 Version: 1.0 Project Definition Material: ACG MTM45-1 Modeling performed for: • Cure Kinetics • Heat Capacity (Cp) • Viscosity 2 Material Description • MTM45-1 is a variable cure temperature, medium…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/cytec-mtm45-1/MTM45-1-Material-Model-Development.pdf

  8. PDF

    NCP-RP-2008-009-Rev-NC-MTM45-1-AS4-145-M-Cure-Cycle

    Report No: NCP-RP-2008-009 Rev N/C Report Date: July 18, 2018 Solvay (Formerly Advanced Composites Group) MTM45-1 / AS4145-32% RW Unitape (12K AS4 UNI) M cure cycle compared to MH cure cycle Equivalency Statistical Analysis Report FAA Special Project Number: SP3505WI-Q NCAMP Document: NCP-RP-2008-009 Rev N/C Report Date: July 18, 2018 Elizabeth Clarkson,…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/cytec-mtm45-1/NCP-RP-2008-009-Rev-NC-MTM45-1-AS4-145-M-Cure-Cycle.pdf

  9. PDF

    NCP-RP-2019-001RevNCMTM45-1AS4-145LHCureCycle

    Report No: NCP-RP-2019-001 Rev N/C Report Date: July 18, 2018 Solvay (Formerly Advanced Composites Group) MTM45-1 / AS4145-32% RW Unitape (12K AS4 UNI) LH cure cycle compared to MH cure cycle Equivalency Statistical Analysis Report FAA Special Project Number: SP3505WI-Q NCAMP Document: NCP-RP-2019-001 Rev N/C Report Date: July 18, 2018 Elizabeth Clarkson,…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/cytec-mtm45-1/NCP-RP-2019-001RevNCMTM45-1AS4-145LHCureCycle.pdf

  10. PDF

    NCP-RP-2009-002-Rev-NC-IM7-LH-cure-cycle-Equivalence-Report-3-21-19

    Report No: NCP-RP-2009-002 Rev N/C Report Date: March 21, 2019 Solvay (Formerly Advanced Composites Group) MTM45-1/IM7-145-32%RW (12K IM7 UNI) LH cure cycle compared to MH cure cycle Equivalency Statistical Analysis Report FAA Special Project Number: SP3505WI-Q NCAMP Document: NCP-RP-2009-002 Rev N/C Report Date: March 21, 2019 Elizabeth Clarkson, Ph.D.…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/cytec-mtm45-1/NCP-RP-2009-002-Rev-NC-IM7-LH-cure-cycle-Equivalence-Report-3-21-19.pdf

  11. PDF

    NCP-RP-2010-002-Rev-NC-MTM45-1-AS4-PW-M-Cure-Equivalency-Statistical-Analysis-Report-3-21-19

    Report No: NCP-RP-2010-002 Rev N/C Report Date: March 21, 2019 Solvay (Formerly Advanced Composites Group) MTM45-1/CF0525-36%RW (3K PW AS4 Fabric) M cure cycle compared to MH cure cycle Equivalency Statistical Analysis Report FAA Special Project Number: SP3505WI-Q NCAMP Document: NCP-RP-2010-002 Rev N/C Report Date: March 21, 2019 Elizabeth Clarkson, …

    https://www.wichita.edu/industry_and_defense/NIAR/Research/cytec-mtm45-1/NCP-RP-2010-002-Rev-NC-MTM45-1-AS4-PW-M-Cure-Equivalency-Statistical-Analysis-Report-3-21-19.pdf

  12. PDF

    NCP-RP-2010-001-Rev-NC-MTM45-1-AS4-PW-LH-Cure-Equivalency-Statistical-Analysis-Report-3-21-19

    Report No: NCP-RP-2010-001 Rev N/C Report Date: March 21, 2019 Solvay (Formerly Advanced Composites Group) MTM45-1/CF0525-36%RW (3K PW AS4 Fabric) LH cure cycle compared to MH cure cycle Equivalency Statistical Analysis Report FAA Special Project Number: SP3505WI-Q NCAMP Document: NCP-RP-2010-001 Rev N/C Report Date: March 21, 2019 Elizabeth Clarkson, Ph.D.…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/cytec-mtm45-1/NCP-RP-2010-001-Rev-NC-MTM45-1-AS4-PW-LH-Cure-Equivalency-Statistical-Analysis-Report-3-21-19.pdf

  13. PDF

    Additional-Documents-2

    HexPly 8552 MATERIAL PROPERTIES DATABASE for use with COMPRO CCA and Raven Created for by David Van Ee & Anoush Poursartip Convergent Manufacturing Technologies, Inc. November 15th, 2009 Hexcel Hexply 8552 Material Properties Characterization TABLE OF CONTENTS OVERVIEW…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/hexcel-8552/Additional-Documents-2.pdf

  14. PDF

    Additional-Documents-3

    …Material Model Development Final Project Wrap-Up Prepared by: A. Shahkarami Reviewed by: D. Van Ee Approved: A.Poursartip Date: November 15th, 2009 Version: 1.0 Project Definition Material: Hexcel 8552 Modeling performed for: • Cure Kinetics • Heat Capacity (Cp) • Viscosity 2 Material Description • HEXPLY 8552 • Material forms received from Hexcel…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/hexcel-8552/Additional-Documents-3.pdf

  15. PDF

    Additional-Documents-1

    Report No: NCP-RP-2013-015 N/C Report Date: May 24, 2013 A Comparison of Equivalence Criteria and Basis Values for HEXCEL 8552 IM7 Unidirectional Tape computed from the NCAMP shared database NCAMP Report Number: NCP-RP-2013-015 N/C Report Date: May 24, 2013 Elizabeth Clarkson, Ph.D. National Center for Advanced Materials Performance (NCAMP) National…

    https://www.wichita.edu/industry_and_defense/NIAR/Research/hexcel-8552/Additional-Documents-1.pdf

  16. PDF

    DurabilityofBondedAircraftStructure-LSmith

    Durability of Bonded Aircraft Structure •   •    •    2 •  •  •  •  3 • • • • 4 • •    •     5 Shear Stress (psi) Status: Static testing of film adhesives complete. EA9696 6000 5000 4000 3000 2000 1000 0 0 0.01 0.02 0.03 Extension (in) Shims for bond line control 0.04 0.05 Status: Two coupons of each film …

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/DurabilityofBondedAircraftStructure-LSmith.pdf

  17. PDF

    JAMS_2025-Development_of_Process_Specifications_for_AFP_Tape_Slitting

    Joint Centers of Excellence for Advanced Materials Development of Process Specifications and Quality Assurance of Slit Tape for Automated Fiber Placement JAMS Technical Review May 2025 Indianapolis, IN Research Team NIAR Principal Investigators: Waruna Seneviratne, PhD & John Tomblin, PhD Slitting Process Development: Alex Martens AFP Process…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/JAMS_2025-Development_of_Process_Specifications_for_AFP_Tape_Slitting.pdf

  18. PDF

    1115_Wednesday_Stevenson

    …Surface Inspection and Post repair Evaluation of Cure State Using Near Infrared Spectroscopy Motivation and Key Issues To help US Aero Space manufacturers of large composite parts produce and maintain a better product in a more cost effective manner Objective To remove some of the qualitative judgements that have to be made concerning composite…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/1115_Wednesday_Stevenson.pdf

  19. PDF

    EffectsofRepairProcedures-Salah

    p Procedures Effects of Repair on Bonded Repairs of Composite Structures 2011 Technical Review John Tomblin, PhD Executive Director, NIAR Lamia Salah Sr. Research Engineer, NIAR FAA Sponsored Project Information ¾ Principal Investigators & Researchers ¾ Dr. John Tomblin, Wichita State University ¾ Lamia Salah, Wichita State University ¾ Mike Borgman,…

    https://www.wichita.edu/industry_and_defense/NIAR/Documents/EffectsofRepairProcedures-Salah.pdf

  20. PDF

    WG4-Working-Group-4-Debrief-Notes

    2024 FAA/EASA Workshop Working Group 4: Part Classification Day 1: WG4 AM Part Classification F3572 − 22 (Standard Practice for Additive Manufacturing – General Principles – Part Classifications for Additive Manufactured Parts Used in Aviation) is the most well-known reference for this topic and has been the reference for WG1 focused on class C & D. 1.…

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