Comparison of the compressive strength of panels with Alclad 24S-T81 sheet or with Alclad 24S-T86 sheet riveted to Alclad 24S-T84 hat-section stiffeners Page: 1 of 14

                                
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4 WE

MR April 1944
1   FEB 148                               -_-_-
NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS
iWA l I ME                                           EP1
ORIGINALLY ISSUED
April 1944 as
Memorandum Report
COMPARISON OF THE COMPRESSIVE STRENGTH OF PANELS WITH
ALCLAD 24S-T81 SHEET OR WITH ALCLAD 211S-T86 SHET
RIVhETED TO ALCLAD 24S -T84 HAT -SECTION STIFFENERS
By Robert A. Weinberger, Carl A. Rossman,
and Gordon P. Fisher
Langley Memorial Aeronautical Laboratory
Langley Field, Va.
WASHINGTON
NACA WARTIME REPORTS are reprints of papers originally issued to provide rapid distribution of
advance research results to an authorized group requiring them for the war effort. They were pre-
viously held under a security status but are now unclassified. Some of these reports were not tech-
nically edited. All have been reproduced without change in order to expedite general distribution.
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