Influence of Martensitic Transformation on the Spall Strength and the Shear Strength of NiTi under Shock Wave Loading in the Temperature Range from 213 K to 413 K

Journal Article · Fri Jul 28 00:00:00 EDT 2006 · AIP Conference Proceedings

DOI:https://doi.org/10.1063/1.2263408· OSTI ID:20875748

Skripnyak, V A; Skripnyak, E G; Dudarev, E F ^[1]; Garkushin, G V ^[2]; Kolobov, Yu R ^[3]

---

1. Tomsk State University, Tomsk, 634050 (Russian Federation)
2. Institute of Problems of Chemical Physics RAS, Chernogolovka, Moscow region, 142432 (Russian Federation)
3. Institute of Strength Physics and Material Sciences, SB RAS, Tomsk, 634055 (Russian Federation)

This article reports new experimental results on the mechanical behavior of the Ni48.9Ti51.1 alloy under shock-wave loading in the temperature range from 213 to 413 K. The samples of NiTi alloy were loaded by impacts of aluminum flyer plates with a thickness of 0.4 mm and an impact velocity of 630{+-}50 m/s. The increase in the yield strength from 0.4 to 2.7 GPa and the spall strength from 1.75 to 3.75 GPa Results indicate that in the range 213 K to 413 K, all values of the spall strength are higher than the values of austenitic NiTi alloys with high contents of nickel. The relationship Us-up for martensitic NiTi demonstrated no anomaly that was observed with austenitic NiTi alloys.

• OSTI ID: 20875748
• Journal Information: AIP Conference Proceedings, Vol. 845, Issue 1; Conference: American Physical Society Topical Group conference on shock compression of condensed matter, Baltimore, MD (United States), 31 Jul - 5 Aug 2005; Other Information: DOI: 10.1063/1.2263408; (c) 2006 American Institute of Physics; Country of input: International Atomic Energy Agency (IAEA); ISSN 0094-243X
• Country of Publication: United States
• Language: English

Related Subjects

75 CONDENSED MATTER PHYSICS
SUPERCONDUCTIVITY AND SUPERFLUIDITY
ALUMINIUM
AUSTENITIC STEELS
FRACTURE PROPERTIES
LOADING
NICKEL
NICKEL ALLOYS
PHASE TRANSFORMATIONS
PLATES
PRESSURE DEPENDENCE
PRESSURE RANGE GIGA PA
SHEAR PROPERTIES
SHOCK WAVES
TEMPERATURE DEPENDENCE
TEMPERATURE RANGE 0273-0400 K
THERMOMECHANICAL TREATMENTS
THICKNESS
TITANIUM ALLOYS
VELOCITY
YIELD STRENGTH