Defense Technical Information Center Compilation Part Notice

Similar documents
This paper is part of the following report: UNCLASSIFIED

Free Energy Simulation of Grain Boundary Segregation and Thermodynamics In Ni3 xal1+x

Phase Transitions Module γ-2: VSM study of Curie Temperatures 1 Instructor: Silvija Gradečak

Defense Technical Information Center Compilation Part Notice

Lecture # 11 References:

Defense Technical Information Center Compilation Part Notice ADP014314

High-resolution electron microscopy of grain boundary structures in yttria-stabilized cubic zirconia

Chapter Outline. How do atoms arrange themselves to form solids?

Lecture # 11. Line defects (1D) / Dislocations

Chapter Outline How do atoms arrange themselves to form solids?

ASTM Conference, May , Hilton Head Island, SC

A rigid model illustrating the formation of misfit dislocations at the (111) diamond/c-bn

Defense Technical Information Center Compilation Part Notice

Single vs Polycrystals

ENGINEERING MATERIALS LECTURE #4

POWDER METALLURGY IMPACT ON THE NANOCRYSTALLINE NiAl PROCESSING

The Science and Engineering of Materials, 4 th ed Donald R. Askeland Pradeep P. Phulé. Chapter 3 Atomic and Ionic Arrangements

Computer Simulation of Nanoparticle Aggregate Fracture

Dislocations and Plastic Deformation

Definition and description of different diffusion terms

Defect in crystals. Primer in Materials Science Spring

(a) Would you expect the element P to be a donor or an acceptor defect in Si?

Chapter Outline Dislocations and Strengthening Mechanisms. Introduction

In this work, the dendrite growth velocity of tetragonal Ni 2 B was measured as a

Ferromagnetic Transitions

STATE OF SOLIDIFICATION & CRYSTAL STRUCTURE

IMPERFECTIONSFOR BENEFIT. Sub-topics. Point defects Linear defects dislocations Plastic deformation through dislocations motion Surface

Figure.1. The conventional unit cells (thick black outline) of the 14 Bravais lattices. [crystallographic symmetry] 1

Chapter 7 Dislocations and Strengthening Mechanisms. Dr. Feras Fraige

Defense Technical Information Center Compilation Part Notice

3, MSE 791 Mechanical Properties of Nanostructured Materials

much research (in physics, chemistry, material science, etc.) have been done to understand the difference in materials properties.

atoms = 1.66 x g/amu

Part II : Interfaces Module 1: Structure of interfaces

E45 Midterm 01 Fall 2007! By the 0.2% offset method (shown on plot), YS = 500 MPa

Point coordinates. x z

Imperfections in the Atomic and Ionic Arrangements

Physcial Metallurgy and Microstructure of Superalloys

Point coordinates. Point coordinates for unit cell center are. Point coordinates for unit cell corner are 111

Fundamental concepts and language Unit cells Crystal structures! Face-centered cubic! Body-centered cubic! Hexagonal close-packed Close packed

Strengthening Mechanisms

The structures of pure metals are crystalline (crystal lattice) with regular arrangement of metal atoms that are identical perfect spheres.

The high temperature decrease of the critical resolved shear stress in nickel-base superalloys

SiC crystal growth from vapor

Multiscale Modeling of Metallic Materials Containing Embedded Particles

Ex: NaCl. Ironically Bonded Solid

Chapter1: Crystal Structure 1

Two marks questions and answers. 1. what is a Crystal? (or) What are crystalline materials? Give examples

Calculated Effect of Alloy Additions on the Saturation Magnetization of Fe 0.80 B 0.20

Twins & Dislocations in HCP Textbook & Paper Reviews. Cindy Smith

VI. THE STRUCTURE OF SOLIDS

"

Point Defects. Vacancies are the most important form. Vacancies Self-interstitials

Defense Technical Information Center Compilation Part Notice

Movement of edge and screw dislocations

Energy and Packing. Materials and Packing

Supplementary Figure 1: Geometry of the in situ tensile substrate. The dotted rectangle indicates the location where the TEM sample was placed.

TEM and Electron Diffraction Keith Leonard, PhD (1999) U. Cincinnati

CHAPTER 3. Crystal Structures and Crystal Geometry 3-1

416 Solid State Physics ; Introduction & Overview

Three stages: Annealing Textures. 1. Recovery 2. Recrystallisation most significant texture changes 3. Grain Growth

4-Crystal Defects & Strengthening

Molecular dynamic simulations of the high-speed copper nanoparticles collision with the aluminum surface

EFFECTS OF ALUMINUM CONTENT AND HEAT TREATMENT ON GAMMA PRIME STRUCTURE AND YIELD STRENGTH OF INCONEL NICKEL-CHROMIUM ALLOY 706

Packing of atoms in solids

Structure factors and crystal stacking

Imperfections in Solids. Imperfections in Solids. Point Defects. Types of Imperfections

Defense Technical Information Center Compilation Part Notice

Enhanced Nucleation Fields due to Dipolar Interactions in Nanocomposite Magnets

1.10 Close packed structures cubic and hexagonal close packing

Order in materials. Making Solid Stuff. Primary Bonds Summary. How do they arrange themselves? Results from atomic bonding. What are they?

Atomic Simulation of Vitrification Transformation in Mg-Cu Thin Film

Objective To study the time and temperature variations in the hardness of Al-4% Cu alloy on isothermal aging.

Chapter 1. Crystal Structure

Additive Element Effects on Electronic Conductivity of Zirconium Oxide Film

Chapter 12 The Solid State The Structure of Metals and Alloys

Energy and Packing. typical neighbor bond energy. typical neighbor bond energy. Dense, regular-packed structures tend to have lower energy.

Structural and magnetic investigations of Sc(Fe 1 x Ni x ) 2 compounds by means of Mössbauer effect and neutron diffraction

Dept.of BME Materials Science Dr.Jenan S.Kashan 1st semester 2nd level. Imperfections in Solids

Slide 1. Slide 2. Slide 3. Chapter 10: Solid Solutions and Phase Equilibrium. Learning Objectives. Introduction

Material Science. Prof. Satish V. Kailas Associate Professor Dept. of Mechanical Engineering, Indian Institute of Science, Bangalore India

Defense Technical Information Center Compilation Part Notice

MACROSTRUCTURE, MICROSTRUCTURE AND MICROHARDNESS ANALYSIS

CRYSTAL STRUCTURE TERMS

Chapter 8 Strain Hardening and Annealing

Recrystallization Theoretical & Practical Aspects

بسم هللا الرحمن الرحیم. Materials Science. Chapter 3 Structures of Metals & Ceramics

Three-dimensional epitaxy: Thermodynamic stability range of coherent germanium nanocrystallites in silicon

Imperfections, Defects and Diffusion

Materials and their structures

CHAPTER 5: DIFFUSION IN SOLIDS

Stacking Oranges. Packing atoms together Long Range Order. What controls the nearest number of atoms? Hard Sphere Model. Hard Sphere Model.

Strengthening Mechanisms

Chapter-3 MSE-201-R. Prof. Dr. Altan Türkeli

The Structure of Materials

ECE440 Nanoelectronics. Lecture 08 Review of Solid State Physics

Molecular Dynamics Simulation on the Single Particle Impacts in the Aerosol Deposition Process

Physics of Materials: Symmetry and Bravais Lattice To understand Crystal Plane/Face. Dr. Anurag Srivastava

Defects and Diffusion

TOPIC 2. STRUCTURE OF MATERIALS III

Transcription:

UNCLASSIFIED Defense Technical Information Center Compilation Part Notice ADP014274 TITLE: Molecular Dynamics Simulations on Nanocomposites Formed by Intermetallic Dispersoids of L1 [2] Type and Aluminum Matrices DISTRIBUTION: Approved for public release, distribution unlimited This paper is part of the following report: TITLE: Materials Research Society Symposium Proceedings Volume 740 Held in Boston, Massachusetts on December 2-6, 2002. Nanomaterials for Structural Applications To order the complete compilation report, use: ADA417952 The component part is provided here to allow users access to individually authored sections )f proceedings, annals, symposia, etc. However, the component should be considered within [he context of the overall compilation report and not as a stand-alone technical report. The following component part numbers comprise the compilation report: ADP014237 thru ADP014305 UNCLASSIFIED

Mat. Res. Soc. Symp. Proc. Vol. 740 Q 2003 Materials Research Society 17.20 Molecular Dynamics Simulations on Nanocomposites Formed by Intermetallie Dispersoids of L1 2 Type and Aluminum Matrices Min Namkung, 'Sun Mok Paik, and Buzz Wincheski NASA Langley Research Center Hampton, VA 23681 'Kangwon National University Chunchun, Korea ABSTRACT Molecular dynamics simulations were performed to characterize the lattice morphology in the region adjacent to the interfaces in nanocomposite systems of a Ni 3 AI dispersoid embedded in Al matrix (Ni 3 AI/AI) and an A1 3 Nb dispersoid embedded in aluminum matrix (Al 3 Nb/AI). A nearly perfect coherent interface is obtained in the AI 3 Nb/AI system with the lattice planes of dispersoid and matrix aligned parallel in all directions. The simulation results show the presence of the matrix atom-depleted regions near the dispersoid boundary for most cases. Detailed analysis revealed that certain sites immediately next to the dispersoid are energetically favored for the matrix atoms to occupy. The matrix atoms occupying these sites attract other atoms producing the depleted regions. In certain specific situations of AI 3 Nb/AI system, however, the wetting of a rotated dispersoid is overwhelmingly complete prompting the need of further study for better understanding. The order parameters of dispersoids calculated for Ni 3 A1 in aluminum is nearly constant while that for A1 3 Nb in aluminum is rapidly decreasing function of temperature in the range of 300 to 1800K. INTRODUCTION Second phase particles that are mixed and uniformly distributed within a matrix are called dispersoids. By selecting appropriate type, size, morphology, and concentration of these dispersoids in a matrix, it may be possible to develop structural components that are capable of actively indicating their physical/chemical states and are optimized for best performance based on given application purpose. For example, the magnetic properties of Ni 3 AI particles can be affected by the local stress states that may be indicative of the changes in other material states. At the same time, when mixed with a substantial volume fraction, the small nearest neighbor distance between such densely populated dispersoids may prevent the dislocation loop formation while being highly resistant to cutting by dislocations [1]. The current series of investigation concentrates on the morphology of such composites to establish a foundation for systematic study on nanocomposite systems of damage indicating capabilities and prolonged service lives. Our previous study clearly showed that a Ni 3 AI dispersoid, which is coherent with the aluminum matrix, causes a substantial degree of local lattice distortion in the vicinity of matrix/dispersoid interface [2] that is known to enhance the strength of alloys [1]. An unresolved problem of the study was the appearance of lattice atom-depleted regions near the interface in the composite system with a rotated dispersoid and its origin was not well understood. Therefore, the purpose of the present study is to find ways of minimizing the 249,

regions of matrix atom depletion near the interface and closely investigate the nature of these regions. The lattice structure of Ni 3 Al is known as L1 2 which possesses a cubic symmetry. Being paramagnetic in nanosize [3], the magnetic field effects of Ni 3 Al particles are not considered in the present simulation. The stable phase of A1 3 Nb is known to be D0 2 2 structure which is tetragonal instead of cubic L 12 [4]. Nevertheless, we choose the metastable L 1 2 phase of A1 3 Nb in the present study for two reasons. First, maintaining the cubic symmetry of the system, the simulation results can be directly compared between the two systems of Ni 3 Al/Al and AI 3 Nb/AI. Second, by varying the physical and chemical states of the metastable system, some unexpected but interesting facts may be found. DETAILS OF SIMULATIONS For each system of Ni3AI/Al and AI 3 Nb/A1, a dispersoid is constructed at the center of a cubic block of pure aluminum. Simulations are first performed by arranging the lattice planes of dispersoid and matrix parallel in all three axes of Cartesian coordinates. Then the dispersoid lattice is rotated with respect to that of the matrix. As an initial investigation of a systematic study on nanocomposites, the rotation of the dispersoids in the present study is limited to the x-y plane and three angles of rotation, i. e., 150, 300 and 45'. Also in this study, the dispersoid lattice spacings are initially set to be very close to their real values, i. e., 0.357 nm for Ni3Al and 0.384 nm for A13Nb compared to 0.405 nm for pure aluminum. The inner radius of matrix and the outer radius of dispersoid are chosen to allow partial overlap between two lattices. The overlapping lattice points are removed to ensure a minimum separation among the atoms in the interface region. With further adjustment of these radii, the two-dimensional dispersoid boundaries in the x-y planes are selected to be Ni-only edges for Ni 3 AI/AI and Al-only for AI 3 Nb. The simulations are performed in the temperature range of 300-1800K based on the temperature-independent parameter values for a modified embedded atom method (EAM) potential given by Baskes [5]. RESULTS AND DISCUSSION Fig. I shows the results of simulations performed at 300 K on the Ni 3 AI/AI system with their lattice planes arranged parallel in all three directions. Shown are the atoms in three planes of (001) centered at z = 0. The hexagons and tiny dots in this figure represent Ni and Al atoms, respectively. Similar results obtained at 900 K are shown in Fig. 2. The presence of the matrix atom-depleted regions around the dispersoid is clear in the results of these two figures. One of the goals of the present study is to find the origin of such matrix atom-depleted regions at the interface, and a simple model has been established and applied to the results of Figs. 1 and 2, as explained in the following. The dispersoids shown in Figs. 1 and 2 are almost octagons and two types of edges are found in their boundaries; those consisting of four nickel atoms and the others consisting of five nickel atoms, which we call the four-atom edges and five-atom edges, respectively, for brevity. Upon a close inspection, one finds that three matrix aluminum atoms are lined up immediately next to the four-atom edges. 250

20 20-... o ooo~ooooo.....,,.;. $;: S... : i i!!i!i! - -10-20 ~... - -20 2-20 -10 0 10 20-20 -10 0 20 X (A) X (A) Figure 1. Simulation results of the Ni3AI/A1 composite system at 300K without rotating the dispersoid. Figure 2. Simulation results of the Ni3A1/AI composite system at 900K without rotating the dispersoid. Fig. 3 shows lattice sites near the interface for the matrix aluminum atoms to occupy. Referring the results of Figs. I and 2, it is clear that the sites A and A's next to a four-atom edge are energetically more favored than B and B' which are next to a five-atom edge. In Fig. 3, one can see that an aluminum atom in site A has four dispersoid Ni atoms, denoted by x, at the nearest neighbor distance. The same applies to an aluminum atom occupying site B. The important difference is that a complete two-dimensional unit cell is formed when an aluminum atom occupies site A. Once this occurs, A' is the next favorite site for occupation since there are four nickel atoms at the nearest neighbor distance and there exists an aluminum atom at site A to lower the energy of site A'. Along the other edge, however, both B and B' sites have to be occupied by two aluminum atoms simultaneously to form a unit cell and such an occurrence has a much lower probability than that of occupying sites A and A' in sequence. In addition, site B' has only two Ni atoms at the nearest neighbor distance and the probability of occupation is even lower for this site. Hence, the matrix aluminum atoms tend to occupy the sites immediately next to the four-atom edges. This argument is based on a two-dimensional picture but it is trivial to extend the logic to a three-dimensional situation. The aluminum atoms executing random motion in the interface region arrive at sites A and A'. Once the aluminum atoms occupy sites A and A', they attract other aluminum atoms causing matrix atom-depleted regions near the other edges of dispersoid boundary. The validity of this argument is supported by the absence of such unit cell formation activity by the matrix aluminum atoms when the symmetry of the system is reduced as shown in the results of Fig. 4 obtained with the dispersoid lattice rotated by 15' about the z-axis. Nevertheless, the strongest evidence for the above argument comes from the results of 45 0 rotation shown in Fig. 5. Here, the five-atom edges are compatible with matrix lattice and the unit cell formation along these edges is clearly seen. Such site preference vanishes at elevated temperature as shown in the simulation results of Fig. 6 for the Ni3AI/A1 system at 900K with the dispersoid rotated by 300 where a significant reduction of the matrix atom depletion is seen. 251

Fig. 7 shows the results of the Al 3 Nb/AI system at 300K obtained without rotating the dispersoid. The system under this situation forms a perfect coherent interface without any noticeable lattice strain in the interface region. Fig. 8 shows the results with the dispersoid rotated by 300 about the z-axis. Here again, the matrix atoms are found to occupy the sites to form unit cells as discussed in the descriptions of the model shown in Fig. 3. The most unexpected results are found for the 150 and 450 rotation cases as seen in Figs. 9 and 10. The two-dimensional shape of the dispersoid in these two figures is much different from that appeared in the results of Figs. 7 and 8. Here, the dispersoid/matrix bonding is A' 0 0 B 10 0 0 0 0o 0 0 B' I.. X - '0.. ". -20-10 0 10 20 x (A) Figure 3. Sites favored (A &A') and Figure 4. Simulation results of the less favored (B & B') by matrix Ni 3 AI/AI system at 300K with the atoms. X is for Ni at z = +a/2, 0 dispersoid rotated by 150 about the z- forni atz=oando foralatz=o. axis. 20-20-.o... 10... -1 0 -.....0-20 -20-20 -in 0 10 20-20 -t0 0 10 20 (A0) x (A) Figure 5. Simulation results of the Figure 6 Simulation results of the Ni 3 AI/AI system at 300K with the Ni 3 A1/A1 system at 900K with the dispersoid rotated by 450 about the z- dispersoid rotated by 30' about the z- axis axis 252

20,... 20.............. 0 - *....... 1.0 100. 0,o o..".....o...."........ ".... -20- -20-20 -10 0 10 20-20 -10 0 10 20 x (A) Figure 7. Simulation results of the Al 3 Nb/Al system at 300K without rotating the dispersoid. o(a) Figure 8. Simulation results of the AI 3 Nb/Al system at 300K with the dispersoid rotated by 300 about the z- axis. 20 20-2............ -20-10 0 10 20-20 -10 0. 0 20 xa Figure 9. Simulation results of the AI 3 Nb/AI composite system at 300K with the dispersoid rotated by 150 about the z-axis. x(a) Figure 10. Simulation results of the AI 3 Nb/AI composite system at 300K with the dispersoid rotated by 450 about the z-axis. complete as if they were interdiffused into each other. Such a change in the dispersoid geometry may or may not be related to the fact that the currently assumed LI 2 structure of Al 3 Ni is a metastable phase. No explanation is available at the moment and systematic study is needed to understand the results of these figures. Finally, the order parameters calculated for systems with unrotated dispersoids over a range of temperature are shown in Figs. 11 and 12 for Ni 3 AI/AI and Al 3 Nb/Al, respectively, It is seen that the Ni 3 A1 dispersoid is thermally stable while Al 3 Nb is not. This is puzzling since the melting temperature is considerably higher in AI 3 Nb than Ni 3 AI (1953K vs. 1673K). The melting behavior of a particle embedded in a matrix can be strongly 253

*NiA" 0 Al] OA18A 0.8 440 0.2 o4 b0 o 0 00 0 0', 0 Tonncnolur (K) Tcor-".a 0 (K) Figure 11. Temperature dependence of order parameters of the unrotated dispersoid and matrix in the Ni 3 AI/AI system. Figure 12. Temperature dependence of order parameters of the unrotated dispersoid and matrix in the A1 3 Nbl/AI system. dependent on the surrounding environment and the temperature dependence of the order parameter needs to be evaluated under various situations to make a general statement. SUMMARY AND CONCLUSION The simulation results of the present study show the general trend of unit-cell formation in the matrix if the lattice planes of the matrix and dispersoid are appropriately aligned. The case of 150 and 450 rotations of the dispersiod atoms produce matrix atom-concentrated and depleted regions near the dispersoid. It was found that a perfectly coherent interface forms between AI 3 Nb and aluminum matrix under appropriate conditions. Also in the A1 3 Nb/A1 system, the dispersoid geometry is significantly changed while its wetting with the matrix remains perfect for particular dispersoid orientations. The underlying mechanism for such perfect wetting needs further systematic study along with the temperature effects and stability of the composite systems. REFERENCES [1]. T. H. Courtney, Mechanical Behavior of Materials, McGraw-Hill (New York, 2000). [2]. M. Namkung, S. Paik and B. Wincheski, On-line Proceeding of International Conference on Computational Nanostructures (ICCN), San Juan, Puerto Rico (April, 2002). [3]. S. N. Kaul and Anita Semwal, "Exchange-enhanced Pauli spin paramagnetism in nanocrystalline Ni 3 AI", Phys. Rev. B 62, 13892 (2000). [4]. M. Yamaguguchi and Inui, in Structural Applications of Internietallic Compound&, edited by J. H. Westbrook and R. L. Fleischer, John Wiley and Sons (New York, 2000). [5]. M. I. Baskes,"Modified EAM potentials for cubic materials and impurities", Phys. Rev. B 46, 2727 (1992). 254