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Compressive strength of corrugated-sheet-stiffened panels for consolidated XB-36 airplane
- Author / Creator
- Available as
- Online
- Summary
-
Compression tests were made of 63 panels stiffened with corrugated sheet. The specimens were constructed from artificially aged Alclad 24S-T aluminum alloy with minimum guaranteed yield strengths o...
Compression tests were made of 63 panels stiffened with corrugated sheet. The specimens were constructed from artificially aged Alclad 24S-T aluminum alloy with minimum guaranteed yield strengths of 57 and 48 kips per square inch for the flat- and corrugated-sheet materials, respectively.
Details
- Creator
- by Robert A. Weinberger, William C. Sperry, and Charles V. Dobrowski
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1944
- Physical Details
-
- 1 online resource (8, [5] pages) : illustrations, photographs
- data file
- OCLC
- on1446381746
- Title from title screen (viewed July 16, 2024)
- NACA Wartime Report L-588.
- Date of issue: January 1944.
- Originally issued as NACA as a Memorandum Report.
- Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
- Includes bibliographical references (page 8)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
Subjects
- Plates (Engineering)
- Sheet-metal, Corrugated.
- Aluminum alloys.
- Materials -- Compression testing.
- Strains and stresses.
- Charts, diagrams, etc.
- aluminum alloy.
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