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Supplement to buckling of long, thin, plywood cylinders in axial compression : experimental treatment

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, Kuenzi, Edward W., and Forest Products Laboratory (U.S.)
Abstract:: Publication restriction has been removed.
Resource Type:: Technical Report
Full Text:: JUL 1 0 7 950 Supplement to PUCICILING THIN, PLYW OD CYLINDERS IN

Inspection of wood aircraft at Salinas, Ecuador, April 4,1943

Creator:: Forest Products Laboratory (U.S.), Teesdale, L. V. (Laurence Victor), and Myer, J. E.
Abstract:: This report is one of a series issued to aid the nation's war program.
Resource Type:: Technical Report
Full Text:: . States Department of Agriculture The members of 7 a party making a survey of the forest resources in

Elastic stability of cylindrical sandwich shells under axial and lateral load

Creator:: Forest Products Laboratory (U.S.) and Haft, Everett Eugene
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Sandwich Construction of the Departments of the Air Force, Navy, and Commerce.
Resource Type:: Technical Report
Full Text:: (8) f l (z)ry r 2 Equation (3) may be integrated to give A r = 7 f (0) f (z)rz _ 2 2 CT , T and

Effect of span-depth ratio and thickness on the mechanical properties of a typical glass-fabric-base plastic laminate as determined by bending tests

Creator:: Forest Products Laboratory (U.S.) and Werren, Fred
Abstract:: This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on Aircraft Design Criteria under the supervision of the Aircraft Committee of the Munitions Board. Information reviewed and reaffirmed July 1955 and 1960.
Resource Type:: Technical Report
Full Text:: -laminate panels were made of 181414 fabric, to a nominal thickness of 1/16 inch (7 plies), 1/4 inch (25

Buckling of long, thin, plywood cylinders in axial compression

Creator:: Forest Products Laboratory (U.S.), March, H. W., Norris, Charles, B. (Charles Brazer), 1894-, and Kuenzi, Edward W.
Abstract:: Information reviewed and reaffirmed, 1962. Original report published in 1943.
Resource Type:: Technical Report
Full Text:: . Jour. Aero. Sciences 7:276, 1940. Also Tsien, H. S. Jour. Aero. Sciences 9:373, 1942. Report No. 1322

Relation of growth characteristics of southern pine to its use in pulping

Creator:: Curran, C. E. (Carleton Edgar), 1890- and Forest Products Laboratory (U.S.)
Resource Type:: Technical Report
Full Text:: ■4 ■Fg•077V 0111 C.tle Ow 64.10 n .'!R,{ AGE-YEARS 7 .m 5prin9wood j) Sample 7

The buckling of flat sandwich panels with either all edges simply supported or all edges clamped

Creator:: Boller, Kenneth H. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed August 1962. Original report dated March 1948.
Resource Type:: Technical Report
Full Text:: corrugated paper . The formula for as given by equations (6) and (7) of Report No . 1525-A, was

Slant driving of nails! Does it pay?

Creator:: Forest Products Laboratory (U.S.)
Resource Type:: Technical Report
Full Text:: N.C., WM M00 0002 COM WW II r+.00 0.02ma0.O,0 0 OAO .,,0 ,A , 0 ..1 N N N.) 4: 4f -,1, g.. FAA 7

Buckling of thin-walled plywood cylinders in torsion

Creator:: Forest Products Laboratory (U.S.), March, H. W., Norris, Charles, B. (Charles Brazer), 1894-, Smith, C. B., and Kuenzi, Edward W.
Abstract:: Information reviewed and reaffirmed August 1960. Original report dated June 1945.
Resource Type:: Technical Report
Full Text:: . = 2e Et sin 8 cos e - 2erm sin a cos 6 + en (cos28 -See equations (1), page 7,. Forest Products

The buckling of flat sandwich panels with edges simply supported (End grain balsa cores and facings of aluminum and glass cloth laminate)

Creator:: Boller, Kenneth H. and Forest Products Laboratory (U.S.)
Abstract:: This report is one of a series issued in cooperation with the Army-Navy-Civil Committee on Aircraft Design Criteria under the supervision of the Aeronautical Board. Information reviewed and reaffirmed January 1954 and 1960.
Resource Type:: Technical Report
Full Text:: -inch aluminum sheet combined with 7/16-inch balsa to 0.032-inch.aluminuM sheet combined with-3/16-inch

Preservation of timber by the steeping process

Creator:: Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed November 1959. Original report dated October 1954.
Resource Type:: Technical Report
Full Text:: higher temperatures may break down the chemicals. Rept. No. 621, revised -7- Table 2.--Approximate

Effect of elevated temperatures of the strengths of small specimens of sandwich construction of the aircraft type

Creator:: Forest Products Laboratory (U.S.) and Kuenzi, Edward W.
Abstract:: This report is one of a series issued in cooperation with Air Force-Navy-Civil Subcommittee on Aircraft Design Criteria under the supervision of the Aircraft Committee of the Munitions Board. Information reviewed and reaffirmed May 1954 and 1962. This report was originally published in August 1949.
Resource Type:: Technical Report
Full Text:: aaD,9,,, R Pg2 t g mzaa E 22 fg: I g aa a ::,..,....,,,- 7: .;gaa g gg gg g a .4'4 a; g_01E

Strength of glued laminated Sitka Spruce made up of rotary-cut veneers

Creator:: Luxford, R. F. (Ronald Floyd), 1889- and Forest Products Laboratory (U.S.)
Abstract:: This report is one of a series issued in cooperation with the Army-Navy-Civil Committee on aircraft design criteria under the supervision of the aeronautical board. Information reviewed and reaffirmed 1962. Original material published 1944.
Resource Type:: Technical Report
Full Text:: shavings, by rotary-cutting the log s into 1/7-inch veneer which would be glued together in suitable

Response of timber joints with metal fasteners to lateral-impact loads

Creator:: Forest Products Laboratory (U.S.) and Jordan, C. A.
Resource Type:: Technical Report
Full Text:: , •• •• •• •• „ •. •• •• •• •• •• .• •• •• •• •• •• •• •• •. ,, tn1, C4 cy. Lo co as 4 co co 0 74. fg (-1 !Et' ,7', .•'..i! e'. 3 3 a.2.,-3 '4' 1

Durability of resin-treated paper honeycomb core

Creator:: Forest Products Laboratory (U.S.) and Boller, Kenneth H.
Abstract:: Information reviewed and reaffirmed in 1965. Original report issued November 1959.
Resource Type:: Technical Report
Full Text:: honeycomb core made_of 125- pound Daft paper, expanded to a honeycomb having 7/16-inch hexagonal cells, and

Supplement to buckling of flat plywood plates in compression, shear, or combined compression and shear : buckling of flat plywood plates in uniform shear with face grain at angled of 0 degrees, +45 degrees, and 90 degrees

Creator:: Voss, Arnold W., Norris, Charles, B. (Charles Brazer), 1894-, Palma, Joseph, and Forest Products Laboratory (U.S.)
Abstract:: Revised July 1950. Information reviewed and reaffirmed 1962.
Resource Type:: Technical Report
Full Text:: -H, Revlsect -7- Specioen lftrn-2 (fig. 1lJ) firtfrer shows this nethod of choosing the buckling

Longitudinally stiffened thin-walled plywood cylinders in axial compression

Creator:: Forest Products Laboratory (U.S.), Kuenzi, Edward W., and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: This report is one of a series issued in cooperation with the Army-Navy-Civil Committee on Aircraft Design Criteria under the supervision of the Aeronautical Board. Information reviewed and reaffirmed March 1956. Original report issued April 1948.
Resource Type:: Technical Report
Full Text:: be expected. hrz 2, 3, 4, 5, 6, 7, plywood cylinders show the constant 1/48-inch veneers 1/8-inch

Stress-strain relations in wood and plywood considered as orthotropic materials

Creator:: Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed March 1956 and 1962. Original report published in 1944.
Resource Type:: Technical Report
Full Text:: treatises on the theory of elasticity and in scientific papers in this field (1), (2), (3), (4), (6), (7

Compression, tension, and shear tests on yellow-poplar plywood panels of sizes that do not buckle with tests made at various angles to the face grain

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and McKinnon, P. F.
Abstract:: Information reviewed and reaffirmed, 1962. Original report published in 1946. This report is one of a series issued in Cooperation with the Army-Navy-Civil Committee on Aircraft Design Criteria under the supervision of the Aeronautical Board.
Resource Type:: Technical Report
Full Text:: described in supplement C agree reasonably well with theory. (7) The ultimate tensile strengths at angles

Effect of prestressing in tension or compression on the mechanical properties of two glass-fabric-base plastic laminates

Creator:: Forest Products Laboratory (U.S.) and Werren, Fred
Abstract:: Information reviewed and reaffirmed April 1957
Resource Type:: Technical Report
Full Text:: section at the center. The maximum sections at the ends were 1-1/2 inches wide and 2-7/8 inches long. The

ScholarsArchive@OSU

Supplement to buckling of long, thin, plywood cylinders in axial compression : experimental treatment

Inspection of wood aircraft at Salinas, Ecuador, April 4,1943

Elastic stability of cylindrical sandwich shells under axial and lateral load

Effect of span-depth ratio and thickness on the mechanical properties of a typical glass-fabric-base plastic laminate as determined by bending tests

Buckling of long, thin, plywood cylinders in axial compression

Relation of growth characteristics of southern pine to its use in pulping

The buckling of flat sandwich panels with either all edges simply supported or all edges clamped

Slant driving of nails! Does it pay?

Buckling of thin-walled plywood cylinders in torsion

The buckling of flat sandwich panels with edges simply supported (End grain balsa cores and facings of aluminum and glass cloth laminate)

Preservation of timber by the steeping process

Effect of elevated temperatures of the strengths of small specimens of sandwich construction of the aircraft type

Strength of glued laminated Sitka Spruce made up of rotary-cut veneers

Response of timber joints with metal fasteners to lateral-impact loads

Durability of resin-treated paper honeycomb core

Supplement to buckling of flat plywood plates in compression, shear, or combined compression and shear : buckling of flat plywood plates in uniform shear with face grain at angled of 0 degrees, +45 degrees, and 90 degrees

Longitudinally stiffened thin-walled plywood cylinders in axial compression

Stress-strain relations in wood and plywood considered as orthotropic materials

Compression, tension, and shear tests on yellow-poplar plywood panels of sizes that do not buckle with tests made at various angles to the face grain

Effect of prestressing in tension or compression on the mechanical properties of two glass-fabric-base plastic laminates

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