Subject Index. Broadgoods, 64 Buffer strips, 5
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1 STP893-EB/Jan Subject Index A Acoustic monitoring (see Monitoring, acoustic) Adhesives BP-907, 211 EC 344, 322 epoxy (see also Composite materials, carbon/epoxy, graphite/epoxy, Kevlar/epoxy, S-glass/epoxy, T-300/epoxy), 26 FM-123-2, 162 FM-300, 322 FM-1000, 266 Narmco 208, 426 rubber-toughened, 26 Aircraft, composite structures,, 34, 48 Angle of lamination, 161 AS 1 graphite/301-6 epoxy composite, 140 AS1 graphite/302 epoxy composite, 26 ASTM Standards D ,427 D , 427 D , 2, 427 D , 2, 427 D D , 2 E 23-82, 369 Bismaleimide, 48 Bolted repairs, 3 B Bond strength (see Strength, bond) Bond thickness, 209 Bonds, adhesive, 266, 322 Boron/aluminum composite, 337 Braided materials (see Composite materials, braided) Broadgoods, 64 Buffer strips, C Cantilevered beam specimens, 64,209, 27, 322 Carbon/epoxy composite, Charpy-type specimens, 368 ASTM Standard E 23-82, 369 Coating, photoelastic, 232 Compact tension specimen, 177 Composite materials AS1/301-6, 140 AS 1/302, 26 AS4-3K/208, 392 boron/aluminate, 337 braided, 392, 404, 422,427 ASTM Standards D , D , D , D ,427 carbon/epoxy, E-glass/polyester, 87 filament-wound, 64 graphite/bismaleimide, 48 graphite/epoxy,, 64, 87, 11,140, 177, 196, 232, 26, 266, 286, 322, 392, Copyrighr ~ 1986 by ASTM International
2 42 COMPOSITE MATERIALS (SEVENTH CONFERENCE) Composite materials (continued) in-lays, reinforcing,, 64, 26, 266 Kevlar/epoxy, 368 metal matrix, 337 multidimensional, 392, 404, 422 orthotropic, 34, 404 quasi-isotropic, 392 S-glass/epoxy, 368 T-300/epoxy, 87, 177, 196, 368 T-300/V-378A, 48 textile (see Composite materials, braided) thermoplastic matrix, 109 thick-wall, 64 unidirectional, 11, 161 Compression failures (see Loads, compression) Computer programs BREPAIR, 34 NASTRAN, 308, 368 Configuration, material, 177 Coupons, 140 Crack, center specimens, 177 Crack propagation (see also Notched specimens) AS 1/302 graphite/epoxy material, 26 cracked-lap shear specimen, 232, 322 resin-toughened matrix, 209 various reinforcing in-layers, 26 Cracked-lap shear specimens, 232, 322 Crack-tip damage (see Damage, cracktip) D Damage circular, 3 crack-tip, 177, 209 impact,, 48, 196 penetration, service-induced, tolerance, 48, 26, 266, 422 various composites, 31 visible versus nonvisible, Data processing (see also Computer programs; Finite element analysis), 163 Debond growth, 322 Defects, manufacturing, in aircraft structures,, 48 Deformation of metal matrices, 337 Delamination adhesive joints, 209 adhesive layers, 266 analysis design, 64, 232 composite joints, 308, 322 filament-wound composites, 64 edge strength, 266, 286 interlaminar shear, 64, 286 reinforcing in-lays, 26 stacking sequence, effect of, 161 stepped-lap joints, 308 thick-wall composites, 64 Double cantilevered beam specimen (DCB) (see Cantilevered beam specimen) Dry test conditions (see Room temperature, dry (RTD)) E Edge strength, 266, 422 Elasticity, braided composite, 392, 404 Electron microscopy, 14, 209, 232, 26 Elevated temperature, wet (ETW),, 48, 140 End-gaps, 308 Fabrication, braided material, 422 Failure mechanisms center-notched boron/aluminum composite, 337 in situ testing, fiber/matrix bond strength, 87
3 SUBJECT INDEX 43 metal composites, 337 threshold in graphite/epoxy composite materials, 196 transverse tensile strain in thermoplastic composites, 109 unidirectional composites, 11 wet graphite/epoxy coupons, 140 Fasteners installation/removal cycles, manufacturing defects, seating depth, Fatigue loads (see Loads, fatigue) Fatigue strength (see Strength, fatigue) Fiber (see also Composite materials) buckling of, 11 glass (see Glass fiber) graphite (see Graphite/epoxy composites) orientation, 404 tow size, 422 volume, 404 Filament-wound composites, 64 Film lamination, resins, 422 Finite element analysis bolted composite repair, 34 bond strength, 87 dynamic/static stress, 368 fracture resistance, 64, interlaminar stress, 266, 308 Flaw size, rocket cases, 64 Flexu'ral specimens, 368 Fracture, interlaminar (see Delamination Fracture mechanisms adhesive joints,, 209 mixed-mode, 64, 140, 232, 322 mode I, 64, 322 mode II, 64, 232 notched/unnotched specimens, 64, 161, 368 thick-wall, filament-wound specimens, 64 wet coupons, 140 Fractographic analysis, 140 Geometric model, 392 Glass fiber buffer strips, mats, 26 polyester in composites, 87, 368 scrim, 26 Global-local laminate variational model, 286 Graphite/bismaleimide composite, 48 Graphite/epoxy composites aircraft structures, braided composites, 392, 404, 422 fiber/matrix systems, 87, 11 filament-wound, 64 interlaminar shear studies, 286 laminate thickness/specimen configuration, 177 mixed mode/mode II interlaminar fracture, 232 notch sensitivity/stacking sequence, 161 projectile impact/tension load studies, 196 use of reinforcing in-lays, 26, 266 wet compression coupons, 140 H HBRF-A resin system, 64 Helical layering, diagram, 72 Hercules AS4-12K graphite, 64, 26 Holes aircraft structure,, 34, 48 loaded/unloaded, 48 strains related to,, 14, 34, 48, 161 Hoop layering, diagram, 72 Humidity (see Water; Wet test conditions) Hygroscopic behavior, composites, 48 I Image analysis, 140 Impact damage (see Damage, impact)
4 44 COMPOSITE MATERIALS (SEVENTH CONFERENCE) Impact loads (see Loads, impact) In-lay materials (see Reinforcing in-lays) In situ test method, 87 Instron testing machine, 339 Interlaminar fracture (see Fracture, interlaminar) Interlaminar shear (see Shear, interlaminar) Isochromatic monitoring (see Monitoring, isochromatic) J-integral, 64 Joints adhesive, 209, 308 lap/strap, 232 metal composite, 308 stepped-lap, 308 strength (see Strength, joint) structural, K Kevlar buffer strips, epoxy composites, 368 mats, 26 Kink band formation, 11 Loads biaxial, bolted composite repairs, 34 thermoplastic composite, 109 compression, aircraft fuselage panels, 18 ASTM Standard D , 12 AS4 graphite/302 epoxy composite, 232 in situ tests various fiber/matrix composites, 87 graphite/epoxy composites, 64, 11, 140 ST-300/1034-C graphite/epoxy composite, 286 thick-wall, filament wound composite, 64 unidirectional composites, 11 wet graphite/epoxy coupons, 140 fatigue, carbon/epoxy composite, graphite/epoxy composite, 48, 196, 322 T-300/V-378A graphite/bismaleimide composite, impact, carbon/epoxy composite, graphite/epoxy composite, 196 Kevlar/epoxy composite, 368 S-glass/epoxy composite, 368 T-300/epoxy composite, 368 shear, aircraft fuselage panels, 19 bolted composite repairs, 34 cracked-lap specimens, 232 global-local laminate model, 286 thick-wall, filament-wound composite, 64 spectrum stepped-lap joints, 308 static carbon/epoxy composite, graphite/epoxy composite, 266, 322 Kevlar/epoxy, 368 S-glass/epoxy, 368 T-300/epoxy, 368 T-300/V-378A composite, tensile boron/aluminum composite, 337 graphite/epoxy composites, 161, 232 strain-energy release rate, 244 transverse strain on thermoplastic matrix, 109
5 SUBJECT INDEX 4 M Manufacturing defects, aircraft structures, Mar-Lin equation, 161 Materials {see Composite materials) Mats, reinforcing in-lay, 26 Metal composite joint, 308 matrix composite, 337 patch, 34 Metallography, 140 Microbuckling, 11 Microdebonding, 87, 11 test apparatus, diagram, 90 Microstructural analysis, 48, 140, 26, 286 Modulus elastic braided composite, 392, 404 FM 1000 adhesive film, 270 tensile braided composite, 400 Moisture {see Water) Monitoring acoustic, 164, 337 emission events, 33 isochromatic, 232 N Nondestructive testing, 19, 29, 87, 140, 180, 232, 286, 337 Northrop ETL standard, 2 Notched specimens, 64, 161, 337, 368 O Optical metallography, 140 Orthotropic composite materials, 34, 368, 404 Panels fatigue-loaded, 18 shear-loaded, 19, 34, 48 Patch, metal, 34 Pattern, braid, 422 Photoelastic coating, 232 Photomicrography, 286 Plate, finite/infinite, 34 Point stress criterion, 161 Poisson's ratio, 64, 112, 117, 270, 40 Polycarbonate, 109 Polyester, 26 Polyetheretherketone, 109 Porosity, aircraft structure, Postbuckling, Projectile impact loads, 196 R Radiographic inspection {see also X- ray analysis) 23, 26 Rail shear test, 64 Reinforcing in-lays broadgoods, 64 buffer strips, FM-1000 adhesive film, 266 glass fiber mat, 26 organic fiber mat, 26 rubber-toughened epoxy, 26 scrim, 26 various in-lays, 28 Repairs, bolted, 34 Residual strength {see Strength, residual) Resins {see also Graphite/epoxy composite) BP-907, 209 epoxy, 11, 209 HBRF-A, 64 impregnation of braided composite, 422 rocket cases, 64
6 46 COMPOSITE MATERIALS (SEVENTH CONFERENCE) HBRF-A (continued) stiff versus soft, 11 Resistance, fracture effect of laminate thickness, 177 filament-wound composite, 64 flexural specimens, 368 interlaminar, 64 Rocket booster case, 64 Room temperature, dry (RTD),, 48, 140, 14 Rubber-toughened adhesive, 26 Scanning electron microscopy (SEM) (see Electron microscopy) Scrim, glass, 26 Shear crippling, 11 Shear, interlaminar, 286, 422 Shear loads (see Loads, shear) Spectrum loading (see Loads, spectrum) Stacking sequence, plies, 161, 196, 286 Static strength (sec Strength, static) Stereology (see Image analysis) Stitching, Strain energy release rate, 64, 266, 407 Strength bearing, 48 bond, 87 compression,, 11, 422 fatigue,, 48 flexural, 422 interfacial, 87 various fiber/matrix systems, 99 joint, notched, 64, 161, 337, 368 residual,, 308 static,, 48, 368 tensile, 392, 422 Stress analysis (see Failure mechanisms; Fracture mechanisms; Loads; Strength) Stress wave propagation, 368 Strip in-lays, reinforcing, T-300/epoxy composite, 87, 177, 196, 368 T-300/V-378A graphite/bismaleimide composite, 48 ASTM Standards D ; ; , 2 Tape, unidirectional, 48 Temperature, elevated, humid effect on aircraft composite structures, effect on AS 1-graphite/301-6 epoxy composite, 140 effect on graphite/bismaleimide composite,' 48 effect on wet graphite/epoxy composite, 140 Temperature, room effect on aircraft composite structures, effect on graphite/bismaleimide, composite, 48 effect on AS 1-graphite/301-6 epoxy composite, 140 Tensile strain (see Loads, tensile) Tension center-crack, 177 compact, 177 Thermoplastic matrix, 109 Thickness bond, 209 laminate, 177 Three-point bend specimen, 177 Tolerance, damange (see Damage tolerance) Toughness, fracture (see Resistance, fracture) Ultrasonic inspection, 19, 29 Unidirectional composites ASTM Standard D , 12 Unidirectional lamination, 11, 161 U
7 SUBJECT INDEX 47 Velocity, projectile, 196 W Water, absorption of, 48 Wet test conditions effect on aircraft composite structures, fiber orientation versus compression failure, 1 effect on graphite/bismaleimide composite, 48 effect on graphite/epoxy composite, 140 X-ray analysis, 180, 286 Yam orientation, 392, 404
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