Mat tested is sandwich structure made of glass-fabric-reinforced phenolic resin honeycomb core and bonded top and bottom to glass-fabric-reinforced phenolic resin facings; laboratory tests indicated that, because of fabrication deficiencies, structural properties of mat were less than considered necessary to withstand required 700 coverages of 50,000-lb single-wheel load with 200-psi tire inflation pressure when mat was placed on uniform subgrade with CBR or 15; results of traffic tests.
Engineering tests of t12 plastic airplane landing mat
U S Waterways Experiment Station -- Tech Report
1961
55 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering tests of T14 plastic airplane landing mat
Engineering Index Backfile | 1967
|Engineering tests of T13 plastic airplane landing mat
Engineering Index Backfile | 1965
|Engineering tests of T13 plastic airplane landing mat
TIBKAT | 1965
|Engineering tests of modified T12 plastic airplane landing mat
Engineering Index Backfile | 1968
|Engineering tests of experimental T11 aluminum airplane landing mat
Engineering Index Backfile | 1963