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High Dynamic Loading of Materials
Part 2
Erhardt Lach
French-German Research Institute of Saint-Louis, ISL
Materials Behaviour under Impact
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Presentation Outline
Classic armour steels(Quenched and tempered steels)
High Nitrogen Steel (HNS)Ausforming steels
Bainitic steelγ-TiAl
Ti-alloyMMC
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Tailoring of mechanical properties of:
Quenched and tempered steels:
by quenching (hardening) and subsequent tempering
Austenitic steels:
work hardening and annealing
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Shielding against low velocity fragmentsHoog K,. Lach E., Maurer R., Rössner H.: Bericht R 134/86
STRAIN
TEN
SILE
STR
ESS
Thickness of the sheet: 3mm
VI = 300 m/s
Under this condition the more ductil steel alloy NAXTRA shows a better performance than the high strength armour steel XH 129
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Classical armour steelsquenched and tempered steels
Micro structure after hot rolling
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0,00,20,40,60,81,01,21,41,6
1000 1200 1400 1600 1800 2000 2200
Em
σdyn,5%, MPa
300 400 500 600HB30
70 mmquenched and tempered steel
Ballistic Tests on Armour Steel
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0
500
1000
1500
2000
2500
0 0,1 0,2 0,3 0,4 0,5 0,6TRUE STRAIN
TRU
E ST
RES
S
C961, 480-530 HB30C963, 370-420 HB30C962, 250-300 HB30
MPa
10 -4 s -1
10 -4 s -1
10 -4 s -1
4500 s -1
4500 s -1
4500 s -1
Dyn. Compression Tests on Armour Steels
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Micro cracks along the white bands, enrichment of carbid brittle behaviour
backside of crater
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Formation of ASB
ASB and micro cracks
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Austenitic steels: Hadfield-Steel
Chem. composition: 13 % Mn und 1.3 % C
metastable austenitic structure
Recommanded for light-weight armour in: MILTECH 5/2007
Initial hardness: 200 HB
After severe deformation: 500 HB
Strongly strain hardening
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0,4
0,6
0,8
1,0
1,2
250 300 350 400 450 500 550 600
Vickershardness HV30
N-c
onte
nt
% %-N
cold workedsolution-annealed
agedworked at 400°C
shock wave hardening
Tailoring of Nitrogen Alloyed Steel
shock wave hardening
cold working:
rolling, forging
heat treatment
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Comparison of HNS and Armour Steel
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0
500
1000
1500
2000
2500
3000
0,0 0,1 0,2 0,3 0,4 0,5 0,6 0,7 0,8
TRUE STRAIN
TRU
E ST
RES
S
solution annealed 280HV30cold worked 380HV30cold rolled 472HV30strain ageing 510HV30
MPa
10 -4 s -12400 s -110 -4 s -1
10 -4 s -1
2000 s -1
4300 s -1
3000 s -1
Compression Test on HNSP900 (0.6 % N)
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0,0
0,4
0,8
1,2
1,6
2,0
2,4
0 200 400 600 800 1000Vickershardness HV30
Fm
a rmour steelcold working steel
P900: cold work hardened
P900 work hardened at 400 ° C
2 3
Cold worked and annealed very brittle under impact condition
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Ballistic Test without Cover Plate and Backing
Target NATO 60°
1. Plate: armour steel, treated to 530 HV30
2. Platte: HNS P900, forged at 400 °C to 500 HV30
The ballistic performance of both plates is identical
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P900 plate after test without cover plate
High density of ASBPlate was impacted in the transient and at the onset of steady state region
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The plate was impacted in the steady state region. Melting of material in ASB‘s.
Nr. 2 at 14
P900 plate after test with cover plate
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Micromechanism of HNS
no formation of deforming martensitemicro structure is absolutely stable
n =n = 0
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0,00,20,40,60,81,01,21,41,61,82,02,22,4
0 500 1000 1500 2000 2500 3000 3500Dyn. Compression Strength(10%)
Fm
MPa
Armor steelColdworking steelP900
forged at 400 °C
coldrolled
Fm vers. dyn. Compression Strength
Nr. 2 at 14
Nr. 3 at 14
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4 mm 3 mm 4 mm
2 mm 3 mm 1 mm 3 mm 2 mm
Layered Armour(japanese sword)
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Very High Hardness Steels
cold working steels
Hot Isostatic Pressed (HIPped)pressureless sinteredmelt metallurgy
In general are these steels are too brittle
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0
500
1000
1500
2000
2500
3000
0 0,1 0,2 0,3 0,4 0,5 0,6 0,7
TRUE STRAIN
TRU
E ST
RES
S
quasistatic dynamic
MPa
armour steelhardness 630 HV30
Compression tests on Mars 300
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Ausforming Steel
ausforming (AFH) and hardening (H)
TIME in s
C
P = perlit noseA = austeniteB = bainiteM = martensiteMs = martensite startC = carbidAc = transition temperature
Tem
pera
ture
in °C
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Ausforming steels
C978: 35NCD16
C979: 45NCD16
(french Norm)
dynamicquasistatic
compression test
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Comparison of high-strength steels
C979: 45NCD16C977: Mars 300 (0.45 C)C978: 35NCD16
flow stress, MPa
Em
dyn. stress at 10% strain
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Formation of ASB in high-strength steels
MARS 300 45NCD16
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0
500
1000
1500
2000
2500
0 0,1 0,2 0,3 0,4 0,5 0,6TRUE STRAIN
TRU
E ST
RES
S
MPa armour steel
rail steel(lower bainit)
Bainitic steels (lower bainit)
dyn compression tests
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0,00,20,40,60,81,01,21,41,61,82,02,2
200 300 400 500 600 700 800 900Hardness HV30
Fm
armour steel
cold working steel
rail steellower bainit
Bainitic steel
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Lower bainit is brittle
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0
500
1000
1500
2000
2500
0,0 0,1 0,2 0,3 0,4 0,5 0,6TRUE STRAIN
TRU
E ST
RES
S
lamellar, quasistaticlamellar, 4000 - 3000 1/sglobular, quasistaticglobular, 4000 - 2500 1/s
MPaTiAl
γ-TiAlCompression test
x 100
lamellar micro
structurex 500
globular micro
structure
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0,00,20,40,60,81,01,21,41,61,82,02,2
200 300 400 500 600 700 800 900Vickershardness HV30
Fm
armour steel
cold working steel
γ -TiAl
globularlamellar
γ-TiAl
After the ballistic test
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0,00,20,40,60,81,01,21,41,61,82,02,22,4
100 200 300 400 500 600 700 800 900
Vickershardness HV30
Fm
Armour steel
Cold working steel
Ti 6 4
Ti 6 4
low cost Ti 6 4
rolled
forged
Ti alloy Ti 6 4
rolled, lamellar micro structure
slow cooling rate
forged, globular micro structure
recrystallisation
x 100 x 500
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Ti 17 alloy (thermomechanical treatment)
specimen 26: ϕ
= 0.7 solution annealing T = 820 °C 4 htempern T = 680 °C 8 h, hardness: 391 HV30
specimen 27: ϕ
= 0.7 solution annealing T = 820 °C 4 h tempern T = 580 °C 8 h, hardness: 463 HV30
specimen 28: ϕ
= 0.9 solution annealing T = 910 °C 1 h tempern T = 560 °C 8 h, hardness: 507 HV30
specimen 29: ϕ
= 0.9 solution annealing T = 910 °C 1 h tempern T = 680 °C 8 h, hardness: 387 HV30
Al Sn Zr Cr Mo O N C H
4.9 2 2.04 4 3.94 0.47 0.004 0.016 0.006
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Different treated Ti 17
x50
initial micro structure specimen 26
x200
x1000
specimen 27
x100 x500
specimen 28 specimen 29
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0
200
400
600
800
1000
1200
1400
1600
0,00 0,02 0,04 0,06 0,08 0,10 0,12TRUE STRAIN
TRU
E ST
RES
S
specimen 26specimen 29specimen 27specimen 28
MPa
Quasistatic tensile test
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0
400
800
1200
1600
2000
2400
0,00 0,05 0,10 0,15 0,20 0,25 0,30 0,35 0,40True Strain
True
Str
ess
26: 391 HV30 27: 463 HV30 28: 507 HV30 29: 387 HV30
MPa
Dyn. Compression Test
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0,00,20,40,60,81,01,21,41,61,82,02,22,4
100 200 300 400 500 600 700 800 900
Vickershardness HV30
Fm
2 9
2 6
2 72 8
armour steels
cold working steels
T i 17 fo rgedinitial status
Ballistic Tests
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Specimen 28
ASB: width = 4 µm
Initial status
ASB: width = 30 µm
Ti alloy Ti17
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Ti 17 specimen 28
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0,0
0,4
0,8
1,2
1,6
2,0
2,4
2,8
0 100 200 300 400 500 600 700 800 900Vickershardness H V30
Fm
Al-Cu5/25% SiCAlSi9M g/20%SiCAlSi7M g0,5/55%SiCAlCu4M g1Ag/55%SiC316L/15%TiB2
armour steel
cold working steelmechanically alloyed
cast
squeeze cast ing
H IP ped
Al-Cu5/25% SiC 316L/15%TiB2
cast AlSi9Mg/20%SiC
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0
100
200
300
400
500
600
700
800
900
AlSi7Mg AlCu5Mg
TRU
E ST
RES
S
20% SiC
55% SiC 25% SiC
MPa
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AlSi7Mg reinforced by 55 - 60 % SiC of size:
F100
106 – 150 µm
F500
5 – 25 µm
F1200
1 – 5 µm
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0
200
400
600
800
0 0,05 0,1 0,15 0,2 0,25TRUE STRAIN
TRU
E ST
RES
S
F100F500F1200
MPa
Matrix: AlSi7Mg
SiCP:
Dynamic Compression Tests
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1,0
1,2
1,4
1,6
1,8
2,0
0 200 400 600 800 1000 1200 1400Particle Size F
EmAlSi7Mg / SiC
F100ρ= 3.0 g/cm3
F500ρ = 3.0 g/cm 3
F1200ρ = 2.7 g/cm 3
Ballistic Tests
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AlSi7Mg reinforced by SiC- particles of size F1200
Gaspressure infiltration
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Submicro Ceramic
Al2 O3 , grain size: 0.6 µm - 9.82 µm
grain-Ø: 0.6 µm grain-Ø: 0.91 µm
grain-Ø: 3.76 µm grain-Ø: 9.82 µm
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Ballistic Test and Materials Properties
grain-Ø yaw
a 0,6 0°
b 3,76 0°
c 9,82 1,8°
d 0,91 0,2°
grain-Øhardness strength
4-point bending test
µm HV10 MPa
a 0,6 1977 ± 32 557 ± 35
b 3,76 1725 ± 22 470 ± 31
c 9,82 1543 ± 46 350 ± 16
d 0,91 1908 ± 15 345 ± 30
Al2 O3
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yaw 1,8 °
Ballistic Tests
hardness / strength
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Ballistic Tests
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