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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:: EUCIKLING LOADS OF FLAT SANDWICH PANELS IN COMPRESSION The I3ucHing

Buckling of flat sandwich panels with all edges clamped

Creator:: Forest Products Laboratory (U.S.) and Boller, Kenneth H.
Abstract:: Information reviewed and reaffirmed August 1962. Original report dated September 1947.
Resource Type:: Technical Report
Full Text:: 5 (r) • 13IJCICLING LOADS Of HAT SANDWICH PANELS IN COMPRESSION

Buckling of flat sandwich panels with loaded edges clamped and the remaining edges simply supported

Creator:: Forest Products Laboratory (U.S.) and Boller, Kenneth H.
Abstract:: Information reviewed and reaffirmed August 1962. Original report dated September 1947.
Resource Type:: Technical Report
Full Text:: FUMING LOADS Of RAT SANDWICH PANELS IN COMPRESSION I3uctlinE of

Buckling of flat sandwich panels with loaded edges simply supported and the remaining edges clamped (Cores of end-grain balsa or cellular cellulose acetate and facings of aluminum or glass cloth laminate)

Creator:: Boller, Kenneth H. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed August 1962. Original report dated September 1947.
Resource Type:: Technical Report
Full Text:: COMPRESSION Pudding of flat Sandwich Panels with Loaded Edges Simply Supported and the Remaining Edges

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:: 13IJCICLINC LOADS Of FLAT SANDWICH PANELS IN COMPRESSION The

Various types of edge conditions

Creator:: March, H. W., Smith, C. B., and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed March 1956 and 1962. Original report published in 1945.
Resource Type:: Technical Report
Full Text:: 13IJCICLING LOADS OF FLAT SANDWICH !PANELS IN COMPRESSION VARIOUS

Preliminary report on the strength of flat sandwich plates in edgewise compression

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.
Resource Type:: Technical Report
Full Text:: facing materials used. in the sandwich plates, anC d.escr ibes the rsethods enployed to obtaia then

Compressive buckling curves for sandwich cylinders having orthotropic facings

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and Zahn, John J.
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Composite Construction for Flight Vehicles of the Departments of the Air Force, Navy, and Commerce.
Resource Type:: Technical Report
Full Text:: sandwich construction is•given in Forest Products Laboratory Report No. 1830. 3 The formulas apply to

Compressive buckling curves for flat sandwich panels with dissimilar facings

Creator:: Forest Products Laboratory (U.S.) and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Composite Construction for Flight Vehicles of the Departments of the Air Force, Navy, and Commerce.
Resource Type:: Technical Report
Full Text:: formulas for use in calculating the buckling of flat, simply supported panels of sandwich construction

Supplement to torsion of sandwich panels of trapezoidal, triangular, and rectangular cross sections : derivation of differential equation and its application to rectangular panels with loads applied at corners

Creator:: Cheng, Shun and Forest Products Laboratory (U.S.)
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Composite Construction for Flight Vehicles of the Departments of the Air Force, Navy, and Commerce.
Resource Type:: Technical Report
Full Text:: Issued in Cooperation with the ANC- 23 PANEL ON COMPOSITE CONSTRUCTION FOR FLIGHT VEHICLES of the

Torsion of sandwich panels of trapezoidal, triangular, and rectangular cross sections

Creator:: Forest Products Laboratory (U.S.) and Cheng, Shun
Abstract:: This report is one of a series issued in cooperation with the ANC-23 panel on composite construction for flight vehicles of the departments of the Air Force, Navy, and Commerce.
Resource Type:: Technical Report
Full Text:: +2n. (1- v2 ) v ) Report No. 1874 -3- Mathematical Analysis The trapezoidal sandwich panel is

Torsion of rectangular sandwich plate

Creator:: Forest Products Laboratory (U.S.) and Cheng, Shun
Abstract:: This report is one of a series issued in cooperation with the ANC-23 panel on composite construction for flight vehicles of the departments of the Air Force, Navy, and Commerce. Original report issued 1959. Information reviewed and reaffirmed 1965.
Resource Type:: Technical Report
Full Text:: (136). III. MATHEMATICAL ANALYSIS (Rigorous Solution) The sandwich plate consisting of two facings

Buckling of simply supported rectangular sandwich panels subjected to edgewise bending

Creator:: Forest Products Laboratory (U.S.), Jahnke, W. E., and Kuenzi, Edward W.
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Composite Construction for Flight Vehicles of the Departments of the Air Force, Navy, and Commerce
Resource Type:: Technical Report
Full Text:: - ( 2 ) Theoretical Considerations Buckling Load If the core of a sandwich construction is

Elastic buckling of a simply supported rectangular sandwich panel subjected to combined edgewise bending and compression

Creator:: Forest Products Laboratory (U.S.) and Kimel, W. R.
Abstract:: Information reviewed and reaffirmed in 1962.
Resource Type:: Technical Report
Full Text:: RECTANGULAR SANDWICH PANEL SUBJECTED TO COMBINED EDGEWISE BENDING AND COMPRESSION* By W. R. KIMEL

Elastic buckling of a simply supported rectangular sandwich panel subjected to combined edgewise bending, compression, and shear

Creator:: Forest Products Laboratory (U.S.) and Kimel, W. R.
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. Information reviewed and reaffirmed 1962. Original report issued November 1956.
Resource Type:: Technical Report
Full Text:: Report is One of a Series Issued in Cooperation with the ANC-23 PANEL ON SANDWICH CONSTRUCTION of the

Elastic buckling of a simply supported rectangular sandwich panel subjected to combined edgewise bending and compression : results for panels with facings of either equal or unequal thickness and with orthotropic cores

Creator:: Forest Products Laboratory (U.S.) and Kimel, W. R.
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. Information reviewed and reaffirmed August 1962. Original report dated November 1956.
Resource Type:: Technical Report
Full Text:: sandwich panel sub- jected to any combination of edgewise bending and compression. Details of mathematical

Compressive buckling curves for sandwich panels with isotropic facings and isotropic or orthotropic cores

Creator:: Forest Products Laboratory (U.S.) and Norris, Charles, B. (Charles Brazer), 1894-
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. Revised January 1958.
Resource Type:: Technical Report
Full Text:: use in computing the buckling of flat panels of sandwich construction under edgewise compressive loads

Stresses induced in a sandwich panel by load applied at an insert

Creator:: Youngquist, W. G., Kuenzi, Edward W., and Forest Products Laboratory (U.S.)
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 1960. Original report issued March 1955.
Resource Type:: Technical Report
Full Text:: Introduction In the use of structural sandwich construction, particularly for aircraft structures, it is often

Flexure of structural sandwich construction

Creator:: Kuenzi, Edward W. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed 1958. Original report issued December 1951.
Resource Type:: Technical Report
Full Text:: Society for Testing Materials Committee C-19, on structural sandwich construction, in Washington, D. C

Effect of shear strength on maximum loads of sandwich columns

Creator:: Forest Products Laboratory (U.S.), Boller, Kenneth H., and Norris, Charles, B. (Charles Brazer), 1894-
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 March 1955 and 1960. Results here reported were obtained during 1950.
Resource Type:: Technical Report
Full Text:: material._ Mathematical Development In dealing with sandwich construction the deflections due to shear

ScholarsArchive@OSU

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

Buckling of flat sandwich panels with all edges clamped

Buckling of flat sandwich panels with loaded edges clamped and the remaining edges simply supported

Buckling of flat sandwich panels with loaded edges simply supported and the remaining edges clamped (Cores of end-grain balsa or cellular cellulose acetate and facings of aluminum or glass cloth laminate)

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

Various types of edge conditions

Preliminary report on the strength of flat sandwich plates in edgewise compression

Compressive buckling curves for sandwich cylinders having orthotropic facings

Compressive buckling curves for flat sandwich panels with dissimilar facings

Supplement to torsion of sandwich panels of trapezoidal, triangular, and rectangular cross sections : derivation of differential equation and its application to rectangular panels with loads applied at corners

Torsion of sandwich panels of trapezoidal, triangular, and rectangular cross sections

Torsion of rectangular sandwich plate

Buckling of simply supported rectangular sandwich panels subjected to edgewise bending

Elastic buckling of a simply supported rectangular sandwich panel subjected to combined edgewise bending and compression

Elastic buckling of a simply supported rectangular sandwich panel subjected to combined edgewise bending, compression, and shear

Elastic buckling of a simply supported rectangular sandwich panel subjected to combined edgewise bending and compression : results for panels with facings of either equal or unequal thickness and with orthotropic cores

Compressive buckling curves for sandwich panels with isotropic facings and isotropic or orthotropic cores

Stresses induced in a sandwich panel by load applied at an insert

Flexure of structural sandwich construction

Effect of shear strength on maximum loads of sandwich columns

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