Design Manual for Impact Damage Tolerant Aircraft Structure. Addendum
Abstract
Contents--Hydrodynamic Ram - Key Design Parameters Influencing Damage Size and Type: Stiffener Attachment, Panel Edge Conditions, Panel Thickness, Projectile Incidence of Impact, Test Fluid, Hybrid Designs, Projectile Shape, Constant Projectile Kinetic Energy and Momentum, Fluid Levels, Stacking Sequence (No Air Flow), Temperature and Moisture, Airflow, Simulation of Ullage; Design Guidelines for Survivable Structure in Combat - Materials and Test Methods; Test Results and Discussion: Characterization of Ballistic Damage in Graphite/Epoxy Laminates, Residual Strength of Ballistic Damaged Graphite/Epoxy, Analysis Verification - Warhead Arena Test; Repairability.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1988
- Accession Number
- ADA196775
Entities
People
- M. J. Jacobson
Organizations
- AGARD