Survey Of Low-alloy Aircraft Steels Heat Treated To High-strength Levels
Report Number: WADC TR 53-254 Part 4
Author: Sachs, George
Corporate Author: Syracuse University
Laboratory: Materials Laboratory
Date of Publication: 1954-08
Pages: 145
Contract: AF 33(616)-392
Project: None Given
PB Number: PB121504
AD Number: AD0045578
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Other options for obtaining this report
Via the Defense Technical Information Center (DTIC): A record for this report, and possibly a full-image download of the report, exists at DTIC Via National Technical Information Service: The NTIS Order Number for this report is: AD045578 This report may have been digitized and made freely available for public download, or made publicly available for purchase by the National Technical Information Service through their online database, the National Technical Reports Library Indications of Public Availability A PB Number, PB121504 , exists for this report, indicating public availability of the report at time of publication No digital image of an index entry indicating public availability is currently available There has been no verification of an indication of public availability from an inside cover statementRelated Reports
This report has the following parts/volumes:
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Survey Of Low-Alloy Aircraft Steels Heat-Treated To High Strength Levels Part 1. Hydrogen Embrittlement
WADC TR 53-254 Part 1 -
Survey Of Low-Alloy Aircraft Steels Heat-Treated To High Strength Levels Part 2. Fatigue
WADC TR 53-254 Part 2 -
Survey Of Low-Alloy Aircraft Steels Heat Treated To High Strength Levels Part 3. Failure Cases
WADC TR 53-254 Part 3 -
Survey Of Low-Alloy Aircraft Steels Heat Treated To High-Strength Levels Part 5. Mechanical Properties In The Presence Of Stress Concentrations
WADC TR 53-254 Part 5 -
Survey Of Low-Alloy Aircraft Steels Heat Treated To High Strength Levels Part 6. Recommendations For Future Research Work On High-Strength Steels
WADC TR 53-254 Part 6