ADVANCED GENERAL AVIATION TRANSPORT EXPERIMENTS

Contents

*   MATERIALS

*   CRASHWORTHINESS

*   ADVANCED MANUFACTURING

*   LIGHTNING

 

 

MATERIALS

*    Material Qualification and Equivalency for Polymer Matrix Composite Material Systems (Updated Sept. 2003)

        [AGATE Statistical Analysis Program (ASAP) 2004 -Version 1]

      Latest versions are available through NCAMP site

     

*    Material Qualification Methodology for 2x2 Biaxially Braided RTM Composite Material Systems

*    Material Qualification Methodology for Field Repair/Wet Layup Composite Material Systems

 

*    B-Basis design Allowables for Epoxy-Based Prepreg: Newport Carbon Plain Weave Fabric 3K70P/NB321

*    B-Basis design Allowables for Epoxy-Based Prepreg: Newport Graphite Unitape G150 NASS/NCT321

*    B-Basis design Allowables for Epoxy-Based Prepreg: Newport E-Glass Fabric 7781/NB321

*    B-Basis design Allowables for Epoxy-Based Prepreg: Cytec (formally 3M) E-Glass Fabric 7781/SP381

*    B-Basis design Allowables for Epoxy-Based Prepreg: Cytec (formally 3M) S-Glass Unitape S2/SP381

*    B-Basis design Allowables for Epoxy-Based Prepreg: Cytec (formally Fiberite) Plain Weave Graphite Fabric T650 3K-70-PW/7740

*    B-Basis design Allowables for Epoxy-Based Prepreg: Cytec (formally Fiberite) Graphite Unitape G30-500 12K/7740

*    B-Basis design Allowables for Epoxy-Based Prepreg: Cytec (formally Fiberite) 8-Harness Graphite Fabric T650 3K-135-8H/7740

*    B-Basis design Allowables for Epoxy-Based Prepreg: Nelcote (formerly FiberCote) Graphite Fabric T300 3KPW/E765

*    B-Basis design Allowables for Epoxy-Based Prepreg: Nelcote (formerly FiberCote) Graphite Unitape T700 24KP/E765

*    B-Basis design Allowables for Epoxy-Based Prepreg: Nelcote (formerly FiberCote) E-Glass Fabric 7781/E765

*    Laminate Design Allowables for Epoxy–Based Prepreg: Nelcote (formerly FiberCote) Graphite Fabric T300 3KPW/E765

*    Laminate Design Allowables for Epoxy–Based Prepreg: Nelcote (formerly FiberCote) Graphite Fabric E765/T300 6K 5HS

*    B-Basis Design Allowables for Wet Layup Field Repair Fiber Reinforced Composite Material Systems: 7781 Glass Fabric/MGS 418

*    B-Basis Design Allowables for Wet Layup/Field Repair Fiber Reinforced Composite Material Systems: 3K Plain Weave Carbon Cloth/MGS 418

*    B-Basis Design Allowables for 2x2 Biaxially Braided RTM Composite Material Systems: Carbon Braid AS4 6K GP/PR520

*    B–Basis Design Allowables for Epoxy–Based Prepreg: Nelcote (formerly FiberCote) Graphite Fabric T300 6K 5HS/E765

*   A–Basis and B–Basis Design Allowables for Epoxy–Based Prepreg: TORAY T700SC-12K-50C/#2510 Plain Weave Fabric [US Units]

*   A–Basis and B–Basis Design Allowables for Epoxy–Based Prepreg: TORAY T700GC-12K-31E/#2510 Unidirectional Tape [US Units]

*   A–Basis and B–Basis Design Allowables for Epoxy–Based Prepreg: TORAY 7781 Finish 558/#2510 Fiberglass Fabric [US Units]

*   A–Basis and B–Basis Design Allowables for Epoxy–Based Prepreg: TORAY T700SC-12K-50C/#2510 Plain Weave Fabric [SI Units]

*   A–Basis and B–Basis Design Allowables for Epoxy–Based Prepreg: TORAY T700GC-12K-31E/#2510 Unidirectional Tape [SI Units]

*   A–Basis and B–Basis Design Allowables for Epoxy–Based Prepreg: TORAY 7781 Finish 558/#2510 Fiberglass Fabric [SI Units]

*   Laminate Design Allowables for TORAY T700G/#2510 Unidirectional Tape, T700S/#2510 Plain Weave Fabric and 7781 Finish 558/#2510 Fiberglass Fabric

 

*   Investigation of Thick Bondline Adhesive Joints

*   Effects of Surface Preparation on Long-Term Durability of Composite Adhesive Bonds

*       Stress Analysis of In-Plane, Shear-Loaded, Adhesively Bonded Composite Joints and Assemblies

 

*      Impact of Aircraft Operation on Composite Airframe Temperatures

      (THERMOD)

 

 

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CRASHWORTHINESS

*    Design and Test of an Improved Crashworthiness Small Composite Airframe

*    Methodology for Seat Design and Certification by Analysis

*    Test Plan - Impact Test of a General Aviation Composite Airframe

*    Estimation of Firewall Loads due to Soft Soil Impact

*    AGATE Composite Airframe Impact Test Results

        (Video 1) (Video 2)

*    Design and Construction of a Crashworthy Composite Airframe

*    Crashworthiness Design Guide Small Airplane Small Airplane

*    Full-Scale Starship Test

 

 

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ADVANCED MANUFACTURING

*    Guide for Low Cost Design and Manufacturing of Composite General Aviation Aircraft

*    Automotive Approaches for General Aviation Aircraft

 

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LIGHTNING

*    Lightning Direct Effects Handbook

 

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Last revised: December 18, 2017

Please direct any questions or comments about the site to: waruna.seneviratne@wichita.edu

 

ADVANCED GENERAL AVIATION TRANSPORT EXPERIMENTS