GENOA Durability and Damage Tolerance, Reliability, Virtual Testing, and Manufacturing For Flight Qualified Structure

Click here to start

Table of Contents

GENOA Durability and Damage Tolerance, Reliability, Virtual Testing, and Manufacturing For Flight Qualified Structure 

GENOA: Progressive Failure Analysis (PFA) 

GENOA Virtual Testing: accurate numerical simulation predicting results of experimental testing 

GENOA Durability and Damage Tolerance: accurate numerical simulation in thermal-mechanical environments of creep, fatigue, and impact 

GENOA Reliability 

GENOA Manufacturing of Perform Composite Net Part Shape 

GENOA Equivalent Laminate Properties and Degradation of 2D/3D Woven/Braided/Stitched Composites 

GENOA software usability 

GENOA innovation encompasses progressive failure simulation by hierarchical modeling of 2D/3D polymeric, ceramic, metallic composites during manufacture, testing, and in the operational environment  

GENOA’s impact: Significantly reduces product development & process costs ( 30% to 50%), reduction of time to market (10 % to 25%), Significantly Improved Product Quality  

FAR Regulatory Consideration for Commercial Aircraft Structure 

A Verified Structural Virtual Design/Analysis Software May Reduce Time and Cost of Test 

Building Block Testing Approach is Accepted for Verifying Structural Certification Performance  

A Verified Structural Virtual Design/Analysis Software may Reduce time and Cost of Test  

GENOA Application / Benefits 

GENOA Virtual Testing Laboratory Software Significantly Reduces the Time and Cost of Testing 

Progressive Failure Simulation & Test Verification of V-Notch/Slotted Shear Coupon 

NASA/LaRC Coupon Correlation 

ACT Phase C Analysis & Design Philosophy in Verification of DSD in S/RFI Commercial Aircraft Wing Structure (Cont’d) 

ACT Phase C Analysis & Design Philosophy in Verification of DSD in S/RFI Commercial Aircraft Wing Structure 

ACT Phase C Analysis & Design Philosophy in Verification of DSD in S/RFI Commercial Aircraft Wing Structure (Cont’d) 

Virtual Testing Correlation With Experiment 

Progressive Failure Simulation & Test Verification Of Mini Space Plane 

Progressive Failure Simulation & Test Verification Of Mini Space Plane 

Progressive Failure Simulation Double Cantilever Beam (DCB) 

CMC Combustor Progressive Failure Analysis Combined Load and Temp (1800°F to 2000°F), After Test Run of 11.5 Hours in JTAGGI+ Engine 

Predicted - Observed Rupture Times for Open-Hole Tension Specimens With 5% Uncertainty in Fiber Strength 

Tested Specimens (Woven PMC) 

GENOA Damage Prediction Modeling Approaches 

Damage Tracking is Expressed in Terms of a Load Displacement Relationship 

14 Damaged Modes Considered In GENOA 

14 Damaged Modes Considered In GENOA (Cont’d)  

14 Damaged Modes Considered In GENOA (Cont’d) 

Bonded Joint Damage Progression Under Cyclic Loading 

Multi Site Fatigue Coupon Damage Analysis 

Multi Site Fatigue IAS Panel Damage Analysis 

Crown Panel Static, and Fatigue Damage Analysis With 38-inch DSD 

GENOA Performed Simulation of Composite Shell Impacted by Engine Blade  

GENOA Performed Simulation of Composite Manufacturing of Textile Preform Blade  

GENOA Performed Simulation of Composite Enhanced Concrete Structure  
 

Author: Alpha Star Corporation 

Email: Info@AlphaStarCorp.com 

Home Page: http://www.AlphaStarCorp.com


 
FeedbackProductsCurrent ResearchPartnersAbout CompanyAlpha STAR Corporation Home Page