Title

Design Allowables for Titanium Alloys

Date

1969

Index Abstract

Not Available

Photo Quality

Complete

Report Number

AFML TR 69-161

Corporate Author

North American Rockwell Corp Los Angeles CA Los Angeles Div

Laboratory

Air Force Materials Laboratory

Extent

388

Identifier

AD0857807

Access Rights

Export Controls

Distribution Classification

1

Contract

AF 33(615)-3979

DoD Project

7381

DoD Task

738106

DTIC Record Exists

Yes

Distribution Change Authority Correspondence

AFSC USAF LTR

Distribution Conflict

No

Abstract

The purpose of this program was to develop design information on four titanium alloys for inclusion into Military Handbook-5. The alloys investigated were Ti-6Al-4V Condition STA, Ti-4Al-3Mo-1V Annealed Condition, Ti-13V-11Cr-3Al Annealed Condition, and Ti-6Al-6V-2Sn Annealed Condition and Condition STA. The mechanical properties investigated were tensile, compression, shear, bearing, fracture toughness and fatigue. The general results obtained are presented in Section VII of this report and the data generated for Military Handbook-5 are presented in Section VIII.

Report Availability

Full text available

Date Issued

1969-06

Provenance

Lockheed Martin Missiles & Fire Control

Creator

Martin, Gardner R.

Sommer, Alfred W.

Type

report

Format

1 online resource