NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
On the Strength of Box Type FuselagesThe present investigation relates to a box-type fuselage with sides consisting of thin smooth sheet metal, stiffened by longitudinal members riveted to the flanged channel-section bulkheads or transverse frames and to the semicircular corrugated corner stiffenings. The results obtained in this particular case can be applied to a great number of similar structures.
Document ID
19930090869
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mathar, J
Date Acquired
September 6, 2013
Publication Date
May 1, 1929
Report/Patent Number
NACA-TM-511
Accession Number
93R20159
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FUSELAGE - BOX - STRENGTH

Related Records

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