Accession Number : ADA196775


Title :   Design Manual for Impact Damage Tolerant Aircraft Structure. Addendum


Corporate Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)


Personal Author(s) : Jacobson, M J


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a196775.pdf


Report Date : Mar 1988


Pagination or Media Count : 34


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.


Descriptors :   *AIRFRAMES , *STRUCTURAL COMPONENTS , AIR FLOW , AMMUNITION DAMAGE , ATTACHMENT , BALLISTICS , DAMAGE , EDGES , EPOXY LAMINATES , FLUIDS , GRAPHITE , IMPACT , KINETIC ENERGY , MOISTURE , MOMENTUM , PANELS , PARAMETERS , PROJECTILES , RESIDUALS , SEQUENCES , SHAPE , SIMULATION , SIZES(DIMENSIONS) , STACKING , STIFFENING , SURVIVABILITY , TEST AND EVALUATION , TEST METHODS , THICKNESS , ULLAGE


Subject Categories : Aircraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE