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Additional static and fatigue tests of high-strength aluminum-alloy bolted joints / by E.C. Hartmann, Marshall Holt, and I.D. Eaton.
- Format:
- Book
- Government document
- Author/Creator:
- Hartmann, E. C., author.
- Holt, M. (Marshall), author.
- Eaton, I. D., author.
- Series:
- Technical note (United States. National Advisory Committee for Aeronautics) ; 3269.
- Technical notes / National Advisory Committee for Aeronautics ; No. 3269
- Language:
- English
- Subjects (All):
- Aluminum alloys--Fatigue.
- Aluminum alloys.
- Bolted joints--Testing.
- Bolted joints.
- Joints (Engineering).
- Strength of materials.
- joints (connections).
- strength of materials.
- Physical Description:
- 1 online resource (42 pages) : illustrations
- Place of Publication:
- Washington [D.C.] : National Advisory Committee for Aeronautics, 1954.
- Summary:
- Additional static and fatigue tests were made on a few types of joints in 75S-T6, 24S-T4, and 14S-T6 high-strength aluminum-alloy extruded bar in order to supplement the data in NACA Technical Note 2276. Comparisons are made with the results of these earlier tests.
- Notes:
- Title from title screen (viewed March 7, 2019).
- "July 1954."
- "Aluminum Company of America."
- No Federal Depository Library Program (FDLP) item number.
- Includes bibliographical references (page 14).
- Print version record.
- Other Format:
- Paper version: Hartmann, E.C. Additional static and fatigue tests of high-strength aluminum-alloy bolted joints
- OCLC:
- 1100474456
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