NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Compressive Strength of 24S-T Aluminum-alloy Flat Panels with Longitudinal Formed Hat-section Stiffeners Having Four Ratios of Stiffener Thickness to Skin Thickness
Document ID
19930082356
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hickman, William A
Dow, Norris F
Date Acquired
August 16, 2013
Publication Date
March 1, 1948
Report/Patent Number
NACA-TN-1553
Accession Number
93R11646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CHARTS - STRESSED SKIN
STRESSED SKIN-STIFFENER COMBINATIONS - BUCKLING
ALUMINUM ALLOYS, SHEET - ALCOA 24ST - STRENGTH, COMPRESSIVE
STIFFENERS, ALUMINUM-ALLOY - ALCOA 24ST HAT-SHAPED
STRESSED SKIN-STIFFENER COMBINATIONS - STRENGTH, COMPRESSIVE
No Preview Available