Download or read book Evaluation of Convair Landing Mat written by Waterways Experiment Station (U.S.) and published by . This book was released on 1964 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Evaluation of Convair Landing Mat written by C. D. Burns and published by . This book was released on 1964 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report describes and gives results of field traffic tests conducted to evaluate two variations of the Convair landing mat: one type has a laminated wood core and the other type an aluminum core. Based on the traffic test results and the observations made during the tests, conclusions are drawn concerning the ability of the mat to perform satisfactorily as a surfacing for runways or taxiways. (Author).
Download or read book Evaluation of Washington Aluminum Company AM2 Landing Mat written by William B. Fenwick and published by . This book was released on 1965 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objectives of the investigation reported herein were to: (a) Evaluate the performance of the Washington AM2 mat under accelerated traffic tests with the wheel loadings contemplated under the SATS concept. (b) Compare the performance of the Washington mat with that of the original experimental AM2 mat designed and fabricated by Harvey. (c) Compare the quality of the extrusions furnished to Washington by Alcoa and Dow Chemical Co.
Download or read book Evaluation of Parameters Affecting Horizontal Stability of Landing Mats written by Yu-Tang Chou and published by . This book was released on 1976 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Evaluation of M9M1 Landing Mat written by Waterways Experiment Station (U.S.) and published by . This book was released on 1963 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Evaluation of Harvey Two piece Landing Mat AM2 written by Cecil D. Burns and published by . This book was released on 1966 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt: The object of the investigation is to evaluate the performance of the Harvey two-piece AM-2 landing mat under accelerated traffic tests. (Author).
Download or read book Evaluation of Three piece AM2 Aluminum Landing Mat written by William N. Brabston and published by . This book was released on 1967 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).
Download or read book Evaluation of Various Sizes of Butler AM1 Landing Mat written by Cecil D. Burns and published by . This book was released on 1966 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: The study was conducted to determine the optimum panel size of the various sizes of AM1 landing mat. The mat was to sustain 1600 operational cycles of an aircraft having a gross weight of 60,000 lb with a single-wheel main-gear-assembly load of 27,000 lb and a 30-7.7 tire inflated to 400 psi. A test section consisting of three items with different subgrade strengths and surfaced with the various sizes of panels was constructed and subjected to accelerated traffic of the 27,000-lb test load with tire inflated to 400 psi. (Author).
Download or read book Evaluation of Harvey Aluminum 1 by 12 ft Extruded Light duty Landing Mat with Symmetrical Butt type End Connectors written by Hugh L. Green and published by . This book was released on 1972 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Evaluation of Butler AM2 Landing Mat written by William B. Fenwick and published by . This book was released on 1966 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: The study was conducted to compare the performance of aluminum landing mat fabricated by Butler Manufacturing Co. The primary method of comparison was by using CBR design curves which were developed to represent 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. CBR design curves were also developed for 1600 passes of a 39,000-lb single-wheel load applied in a single track to represent the calculated loading imposed on the landing mat during launching of the 60,000-lb aircraft by catapult. (Author).
Download or read book Evaluation of Dow Chemical Extruded Aluminum Landing Mat XM18E1 written by Dewey W. White and published by . This book was released on 1969 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Evaluation of Kaiser MX19 B and MX19 C Aluminum Honeycomb Landing Mat written by Gordon L. Carr and published by . This book was released on 1973 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Evaluation of Various Sizes of Harvey Aluminum AM2 Landing Mat written by William B. Fenwick and published by . This book was released on 1966 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: This investigation was conducted to determine the optimum panel size for the AM2 mat fabricated by Harvey Aluminum Company, Torrance, Calif. The basic AM2 mat was designed to sustain 1600 operational cycles of an aircraft having a gross weight of 60,000 lb with a single-wheel main-gear-assembly load of 27,000 lb and a 30-7.7 tire inflated to 400 psi. A test section consisting of three items with different subgrade strengths and surfaced with three different size mat panels was constructed and subjected to 188 coverages (equivalent to 1600 cycles of aircraft operations) of accelerated traffic of a 27,000-lb single-wheel load with a 30-7.7 tire inflated to 400 pri. The mat was also tested for its ability to sustain 1600 passes of a 39,000-lb single-wheel load applied in a single track to represent the calculated loading that would be imposed on a landing mat during launching of a 60,000-lb aircraft by catapult.
Download or read book Engineering Tests of Experimental T11 Aluminum Airplane Landing Mat written by D. N. Brown and published by . This book was released on 1966 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Evaluation of Harvey Modified AM2 Landing Mat written by William B. Fenwick and published by . This book was released on 1965 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Evaluation of AM 2 Mod 5 Production Landing Mat written by Charles W. Dorman and published by . This book was released on 1986 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Evaluation of Dow Chemical Company Extruded Aluminum 4 piece 4 by 4 ft Landing Mat MX18 E written by Dewey W. White and published by . This book was released on 1973 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: