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A model study of landing mat subjected to C-5A loadingsThe 1.22 x 1.37 m mat runway in the standard brick pattern with transverse hinged joints is more stable and less susceptible to a buckling failure than the 0.60 x 2.74 m mat runway. Use of tension anchors appears to be a feasible means of controlling longitudinal displacement of the runway and potential runway buckling. Anchors appear to be a practical means to reduce maintenance on mat runways. The 1.22 x 1.37 m mat in the alternate brick pattern or the 90 deg rotated standard brick pattern forms a dynamically more stable runway with a high resistance to buckling failure. The runway in these patterns is much stiffer and longitudinal movement was less than for the standard brick pattern. The model 1.22 x 1.37 m alternate brick pattern runway was difficult to assemble and extremely difficult to take apart.
Document ID
19770003321
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blotter, P. T.
(Utah State Univ. Logan, UT, United States)
Kiefer, F. W.
(Utah State Univ. Logan, UT, United States)
Christiansen, V. T.
(Utah State Univ. Logan, UT, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: NASA. Langley Res. Center Advan. in Eng. Sci., Vol. 1
Subject Category
Structural Mechanics
Accession Number
77N10263
Funding Number(s)
CONTRACT_GRANT: F29601-73-C-0131
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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