Development of CBR Design Curve for M9M2 Landing Mat PDF Download
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Author: Waterways Experiment Station (U.S.)
Publisher:
ISBN:
Category : Landing mats
Languages : en
Pages : 114
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Book Description
Author: Waterways Experiment Station (U.S.)
Publisher:
ISBN:
Category : Landing mats
Languages : en
Pages : 114
Get Book Here
Book Description
Author: Waterways Experiment Station (U.S.)
Publisher:
ISBN:
Category : Landing mats
Languages : en
Pages : 92
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Book Description
Author: Cecil D. Burns
Publisher:
ISBN:
Category : Landing mats
Languages : en
Pages : 70
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Book Description
Author: United States. Army. Corps of Engineers
Publisher:
ISBN:
Category :
Languages : en
Pages : 130
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Book Description
Author: U.S. Army Engineer Waterways Experiment Station
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 430
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Book Description
Author: Waterways Experiment Station (U.S.)
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 322
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Book Description
Author: William B. Fenwick
Publisher:
ISBN:
Category : Landing mats
Languages : en
Pages : 66
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Book Description
This investigation was conducted to evaluate a modified and connector on the AM2 landing mat fabricated by Harvey Aluminum, Inc., Torrance, Calif. A test section, consisting of three clay subgrade items with different strengths and one sand item, was constructed and surfaced with the modified AM2 mat. The test section was subjected to traffic representing 1600 operational cycles of an aircraft having a 60,000-lb gross weight with a single-wheel main-gear assembly load of 27,000 lb and a 30-7.7 tire inflated to 400 psi.
Author: Waterways Experiment Station (U.S.)
Publisher:
ISBN:
Category : Landing mats
Languages : en
Pages : 60
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Book Description
Author: William N. Brabston
Publisher:
ISBN:
Category : Landing mats
Languages : en
Pages : 90
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Book Description
The investigation was conducted to evaluate three-piece AM2 landing mat. The mat was fabricated from three 8-in.-wide extrusions welded together to form a 2-ft-wide plank. A test section consisting of one sand item and three clay subgrade items with various CBR strength values was constructed and surfaced with the three-piece mat. The test section was subjected to uniform-coverage and single-line traffic representing operations of an aircraft having a 60,000-lb gross weight with a single-wheel main gear assembly load of 27,000 lb with a 30.7.7 tire inflated to 400 psi. (Author).
Author: Cecil D. Burns
Publisher:
ISBN:
Category : Landing mats
Languages : en
Pages : 50
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Book Description
