NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Column and Plate Compressive Strengths of Aircraft Structural Materials: 24S-T Aluminum-alloy Sheet
Document ID
19930093380
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Wartime Report
Authors
Lundquist, Eugene E. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Schuette, Evan H. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Heimerl, George J. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Roy, J. Albert (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1945
Report/Patent Number
NACA-ARR-L5F01
NACA-WR-L-190
Report Number: NACA-ARR-L5F01
Report Number: NACA-WR-L-190
Accession Number
93R22670
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COLUMNS - INSTABILITY
DIAGRAMS, STRESS-STRAIN
ALUMINUM ALLOYS, SHEET - ALCOA 24ST - STRENGTH, COMPRESSIVE
COLUMNS, ALUMINUM-ALLOY - ALCOA 24ST - STRENGTH
PLATES - STRENGTH, COMPRESSIVE
CHANNELS

Related Records

There are no records associated with this record.
No Preview Available