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T1240_UW_Lin

…Styuart Department of Aeronautics and Astronautics University of Washington July 21, 2009 The Joint Advanced Materials and Structures Center of Excellence FAA Sponsored Project Information • Principal Investigator: • Dr. Kuen Y. Lin, Aeronautics and Astronautics, UW • Research Scientist: Dr. Andrey Styuart, UW • Pre-Doctoral Research Assistant: Chi Ho…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/T1240_UW_Lin.pdf

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NMS-085-Slash-1-Rev-A-Material-Spec-15-2021

…up to 240 canisters of filament per filament lot. Filament lot information is listed in the material Certificate of Conformance. Limits computed at α=0.01 and modified CV. Specimens should be printed on the five different build platform location. Specimens are dried at 250°F±5°F for 24 hours minimum. (3) Specimens are printed per “D638_XZ_T16A.cmb”, it is …

https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-085-Slash-1-Rev-A-Material-Spec-15-2021.pdf

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

…specifications may be able to do so by demonstrating the capability to reproduce the original material properties; a process known as equivalency. More information about this equivalency process including the test statistics and its limitations can be found in Section 6 of DOT/FAA/AR-03/19 and Section 8.4.1 of CMH-17-1G. This specification is developed…

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

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JAMS-Boeing-feedback_07-12-07

…the phase the project is in (just starting, midpoint, complete, etc) – so the audience can have a sense of what to expect. Some of the papers were presented so quickly, with information so dense, that the value of the material was diminished. 2 Areas of Interest to Boeing Engineering, Operations & Technology | Phantom Works Evaluation of NDI…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/JAMS-Boeing-feedback_07-12-07.pdf

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NMS-085-Rev-C-Base-Material-Spec-1-15-2020

…of Thermoplastics by Extrusion Plastometer Standard Test Methods for Flexural Properties of Unreinforced and Reinforced Plastics and Electrical Insulating Materials Standard Test Methods for Constituent Content of Composite Materials Standard Test Method for Determination of Moisture in Plastics by Relative Humidity Sensor Standard Test Method for…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-085-Rev-C-Base-Material-Spec-1-15-2020.pdf

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JMADD_and_JMADX-SAMPE_2025_v2

…in JMADD is 0.1 in/in/min. and AMS7028 were tested using 0.05 in/in/min. Comparisons are only for informational purposes. T99 and T90 calculated omitting specimens fabricated by ATI powder lot 12. Oxygen (wt%) was below 0.11% (out of specification per AMS 7015) DISTRIBUTION STATEMENT A. Approved for public release: Distribution is isunlimited. 16May…

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

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EvaluationofNotchSensitivityinCompositeSandwicStructures-DAdams

Evaluation of Notch Sensitivity in Composite Sandwich Structures Dan Adams Marcus Stanfield Brad Kuramoto University of Utah 2015 Technical Review FAA Sponsored Project Information • Principal Investigators: Dr. Dan Adams Dr. Mike Czabaj • Graduate Student Researchers: Marcus Stanfield Brad Kuramoto • FAA Technical Monitor: Lynn Pham • Primary…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/EvaluationofNotchSensitivityinCompositeSandwicStructures-DAdams.pdf

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W1240_Raju

…(in progress) Wichita State University The Joint Advanced Materials and Structures Center of Excellence 4 FAA Sponsored Project Information • Principal Investigators & Researchers – K.S. Raju – J.F. Acosta, N. Pratap, K.Y. Tan, S. Elyas, M. Siddiqui • FAA Technical Monitor – Alan Abramowitz • Other FAA Personnel Involved – Curtis Davis •…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/W1240_Raju.pdf

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1320-Quick-Hit-America-Makes-Martin

…(SDOs)  Avoid duplication of effort  Encourage liaisons between SDOs  Provide subject matter experts to help SDOs develop the standards  Better inform decision-making on resource allocation for standards participation and R&D needs  Clarify the current and desired future standardization landscape  Establish a common framework of AM…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/1320-Quick-Hit-America-Makes-Martin.pdf

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800_Thursday_Raju

…SANDWICH STRUCTURES J.S. Tomblin & K.S. Raju National Institute for Aviation Research The Joint Advanced Materials and Structures Center of Excellence FAA Sponsored Project Information • Principal Investigators & Researchers – J.S. Tomblin – K.S. Raju, J. Dietiker – J. Bakuckas • FAA Technical Monitor – Curtis Davis • Other FAA Personnel Involved…

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

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1245_Tuesday_Salah

…process parameter deviation to the performance of bonded repairs ¾ To provide information on repair damage tolerance depending on the area where the damage was inflicted ¾ To identify the crucial steps in bonded repair ¾ To develop rigorous repeatable repair processes that ensure structural integrity of bonded repairs ¾ To gain confidence in bonded…

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

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W0800_UW_TuttleFeraboli

…Simplify certification of discontinuous fiber composite aircraft parts The Joint Advanced Materials and Structures Center of Excellence 7 Project Information • Personnel Involved: University of Washington: Paolo Feraboli, Tyler Cleveland, Marissa Morgan (A&A Dept) Mark Tuttle, Paul Labossiere, Tory Shifman (ME Dept) Hexcel (principally): Bruno…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/W0800_UW_TuttleFeraboli.pdf

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NMS-451-12-Rev-E-Aug-18-2021-MTM45-1-6781

…generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 Medium Temperature, Out-of-Autoclave, Oven-Vacuum-Bag Cure Epoxy Resin Impregnated Fiber Reinforced Composite Materials, Type 35, Class 4, Grade 298, Style 6781 Solvay (Formerly Cytec, Umeco Structural Materials (USM-OK), The Advanced Composites Group (ACG)) MTM45-1 6781…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-451-12-Rev-E-Aug-18-2021-MTM45-1-6781.pdf

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300_Tuesday_Livne

…cases Goals: Identify worst case damage and structural variation scenarios and critical areas Provide flutter information for Monte Carlo (or other) statistical simulations University of Washington 7 Automated System for Calculating Flutter Speeds of Large Numbers of Airframe Structural Variations University of Washington 8 Reduction in flutter…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/300_Tuesday_Livne.pdf

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330_Wednesday_Siegmund

…supporting development of models Purdue University – Joint Advanced Materials and Structures Center of Excellence 2 FAA Sponsored Project Information • Principle Investigators & Researchers – Hyonny Kim (now at UCSD) – C. T. Sun – Thomas Siegmund – Post-Doc: Steffen Brinkmann – Students: Haiyang Qian, Nicholas Girder, Matt Wan • former…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/330_Wednesday_Siegmund.pdf

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CMH17-STATS_final

… input Diagnostic tests at individual conditions Output ﬁle contains input and results Double precision math Special Introductory Pricing Available For more information, visit https://www.niar.wichita.edu/cmh17/StatisticsSoftware.aspx CMH-17 is a division of Wichita State University.

https://www.wichita.edu/industry_and_defense/NIAR/Documents/CMH17-STATS_final.pdf

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Damage_Tolerance_Test_Method_Development_for_Sandwich_Composites-Adams

Damage Tolerance Test Method Development for Sandwich Composites 2013 Technical Review Brad Kuramoto and Dan Adams University of Utah FAA Sponsored Project Information • Principal Investigator: Dr. Dan Adams • Graduate Student Researcher: Brad Kuramoto • FAA Technical Monitor: David Westlund • Collaborators: ASTM Committee D30 Boeing Materials Sciences …

https://www.wichita.edu/industry_and_defense/NIAR/Documents/Damage_Tolerance_Test_Method_Development_for_Sandwich_Composites-Adams.pdf

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

…capability to reproduce the original material properties; a process known as equivalency. More information about this equivalency process including the test statistics and its limitations can be found in Section 6 of DOT/FAA/AR-03/19 and Section 8.4.1 of CMH-17-1G. This specification is developed based on the material properties that are available…

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

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840_Tuesday_Ilcewicz

…AIR Report • International standard • Unofficial FAA to describe essential document for course content informational • Drafted & approved by CACRC purposes only • Formal reference that is archived • Written by FAA (L. Cheng & L. Ilcewicz) • Not a formal reference that is archived Import Industry Interface, CMH-17 Key FAA JAMS Technical Report • FAA…

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

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NMS-451-4-Rev-D-Aug-18-2021-MTM45-1-7781

…generated and maintained in accordance with NCAMP Standard Operating Procedures, NSP 100 Medium Temperature, Out-of-Autoclave, Oven-Vacuum-Bag Cure Epoxy Resin Impregnated Fiber Reinforced Composite Materials, Type 35, Class 4, Grade 293, Style 7781 Solvay (Formerly Cytec, Umeco Structural Materials (USM-OK), The Advanced Composites Group (ACG)) MTM45-1 7781…

https://www.wichita.edu/industry_and_defense/NIAR/Documents/NMS-451-4-Rev-D-Aug-18-2021-MTM45-1-7781.pdf