Title

Surface And Interfacial Effects In Relation To Brittleness In Refractory Metals

Date

1966

Index Abstract

Not Available

Photo Quality

Complete

Report Number

AFML TR 65-226

Creator

Fourdeux, A.

Rueda, F.

Votava, E.

Wronski, A.

Corporate Author

Union Carbide European Research Associates

Laboratory

Air Force Materials Laboratory

Extent

154

Identifier

AD0486445

Access Rights

Export Control

Distribution Classification

1

Contract

AF 61(052)-774

DoD Project

7351 - Metallic Materials

DoD Task

735101

DTIC Record Exists

No

Distribution Change Authority Correspondence

USAFML LTR

Distribution Conflict

No

Abstract

An experimental program was conducted to compare the mechanical properties of high purity and impure niobium and the mechanical properties of high purity tungsten, both in polycrystalline and single crystal forms. Slip in high purity niobium takes place on the (110) planes in the (111) directions and yielding is governed by the conservative motion of jogs in screw dislocations, rather than by the unlocking of dislocations from the interstitial impurity cloud. Between the upper and lower yield points there is a sudden generation of a large number of dislocations by double cross-slip mechanism. High purity niobium has greater ductility, higher uniform elongation, increased work hardening, but lower strength than impure niobium. Further, it has a yield point in the temperature range 20 C to 800 C. Appreciable ductility can be achieved at room temperature in commercially pure tungsten, but the mechanical properties are strongly orientation dependent. The ductile-to-brittle transition temperature is about 100 C higher sintered material than in melted material which is of coarser gran size and probably higher purity. Very high purity polycrystalline tungsten was found to show some ductility down to -196 C in the recrystallization condition. However, the fracture process is controlled to a considerable extent by grain boundaries in the temperature range +200 C to -196 C.

Report Availability

Full text available

Date Issued

1966-04

Provenance

Lockheed Martin Missiles & Fire Control

Type

report

Format

1 online resource