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DOT-FAA-AR-00-47.pdf View Download |
Material Qualification and Equivalency for Polymer Matrix Composite Material Systems |
793k |
v. 2 |
May 5, 2009, 6:46 AM
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Richard Abbott |
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DOT-FAA-AR-00-74.pdf View Download |
Assessment of Probabilistic Certification Methodology for Composite Structures |
584k |
v. 2 |
May 5, 2009, 6:46 AM
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Richard Abbott |
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DOT-FAA-AR-01-55.pdf View Download |
Probabilistic Design of Damage Tolerant Composite Aircraft Structures |
5475k |
v. 2 |
May 5, 2009, 6:46 AM
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Richard Abbott |
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DOT-FAA-AR-02-101.pdf View Download |
Damage Tolerance Characterization of Sandwich Composites Using Response Surfaces |
2242k |
v. 2 |
May 5, 2009, 3:05 PM
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Richard Abbott |
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DOT-FAA-AR-02-121.pdf View Download |
Guidelines for Analysis, Testing, and Nondestructive Inspection of Impact-Damaged Composite Sandwich Structures |
8591k |
v. 2 |
May 5, 2009, 5:48 PM
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Richard Abbott |
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DOT-FAA-AR-03-74.pdf View Download |
Bonded Repair of Aircraft Composite Sandwich Structures |
3956k |
v. 2 |
May 5, 2009, 7:30 AM
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Richard Abbott |
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DOT-FAA-AR-04-16.pdf View Download |
Uncontained Engine Debris Analysis Using the Uncontained Engine Debris Damage Assessment Model |
2561k |
v. 2 |
May 5, 2009, 7:30 AM
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Richard Abbott |
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DOT-FAA-AR-06-9.pdf View Download |
Statistical Testing of Aircraft Materials for Transport Airplane Rotor Burst Fragment Shielding |
3921k |
v. 2 |
May 5, 2009, 5:50 PM
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Richard Abbott |
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DOT-FAA-AR-95-109.pdf View Download |
Comparative Evaluation of Failure Analysis Methods for Composite Laminates |
3034k |
v. 2 |
May 5, 2009, 6:47 AM
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Richard Abbott |
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DOT-FAA-AR-99-24.pdf View Download |
Structural Integrity of Discontinuous Stiffeners Integrally Braided and Woven Composite Panels |
2096k |
v. 2 |
May 5, 2009, 6:48 AM
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Richard Abbott |
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DOT-FAA-AR-99-2.pdf View Download |
Probabilistic Design Methodology for Composite Aircraft Structures |
1280k |
v. 2 |
May 5, 2009, 6:47 AM
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Richard Abbott |
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DOT-FAA-AR-99-49.pdf View Download |
Review of Damage Tolerance for Composite Sandwich Airframe Structures |
1424k |
v. 2 |
May 5, 2009, 6:48 AM
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Richard Abbott |
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NASA-CR-208994.pdf View Download |
Facesheet Wrinkling in Sandwich Structures |
621k |
v. 2 |
May 5, 2009, 7:12 AM
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Richard Abbott |
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NASA-CR-209343.pdf View Download |
Validated Feasibility Study of Integrally Stiffened Metallic Fuselage Panels for Reducing Manufacturing Costs |
372k |
v. 2 |
May 5, 2009, 7:13 AM
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Richard Abbott |
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NASACR-2218-1.pdf View Download |
Analysis and Design of Advanced Composite Bonded Joints |
3783k |
v. 5 |
May 5, 2009, 6:54 AM
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Richard Abbott |
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NASA-CR-4736.pdf View Download |
Cost Optimization Software for Transport Aircraft Design Evaluation |
9097k |
v. 2 |
May 5, 2009, 7:14 AM
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Richard Abbott |
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NASA-CR-4750.pdf View Download |
Handbook of Analytical Methods for Textile Composites |
2289k |
v. 2 |
May 5, 2009, 7:15 AM
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Richard Abbott |
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NASA-TM-104060.pdf View Download |
Non-dimensional Parameters and equations for buckling of Symmetrically laminated thin elastic Shallow Shells |
2601k |
v. 2 |
May 5, 2009, 7:16 AM
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Richard Abbott |
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NASA-TM-110204.pdf View Download |
Structural Test Documentation and Results for the McDonnell Douglas All-Composite Wing Stub Box |
1496k |
v. 2 |
May 5, 2009, 7:16 AM
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Richard Abbott |
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NASA-TM-110267.pdf View Download |
Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box |
1520k |
v. 2 |
May 5, 2009, 7:17 AM
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Richard Abbott |
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NASA-TM-110309.pdf View Download |
Evaluation of a Composite Sandwich Fuselage Side Panel With Damage and Subjected to Internal Pressure |
696k |
v. 2 |
May 5, 2009, 7:17 AM
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Richard Abbott |
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NASA-TM-110331.pdf View Download |
Fatigue Debonding Characterization in Composite Skin/Stringer Configurations |
1634k |
v. 2 |
May 5, 2009, 7:18 AM
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Richard Abbott |
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NASA-TM-210844.pdf View Download |
An Assessment of the State-of-the-Art in the Design and Manufacturing of Large Composite Structures for Aerospace Vehicles |
5282k |
v. 2 |
May 5, 2009, 7:18 AM
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Richard Abbott |
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NASA-TN-D-8257.pdf View Download |
Minimum Mass Design of Filamentary Composite Panels Under Combined Loads: Design Procedure Based on Simplified Buckling Equations |
1324k |
v. 2 |
May 5, 2009, 7:19 AM
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Richard Abbott |
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NASA-TP-3568.pdf View Download |
Buckling Behavior of Long Anisotropic PlatesSubjected to Combined Loads |
1086k |
v. 2 |
May 5, 2009, 7:22 AM
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Richard Abbott |
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NASA-TP-3587.pdf View Download |
Buckling and Postbuckling Behavior of Laminated Composite Plates With a Cutout |
230k |
v. 2 |
May 5, 2009, 7:22 AM
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Richard Abbott |