Index Catalog // ScholarsArchive@OSU

Supplement no. 2 to 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 ANC-23 Panel on Sandwich Construction of the Departments of the Air Force, Navy, and Commerce. Information reviewed and reaffirmed 1962. Original report issued February 1956.
Resource Type:: Technical Report
Full Text:: that the formulas are also satisfactory for use in the design of sandwich structures in which the load

Cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear

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 1956 and 1962. Original report issued October 1948.
Resource Type:: Technical Report
Full Text:: FATIGUE OF SANDWICH CONSTRUCTIONS FOR AIRCRAFT Cellular-hard

Compressive and shear properties of two configurations of sandwich cores of corrugated foil

Creator:: Forest Products Laboratory (U.S.) and Stevens, Gordon H.
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 CORES OF CORRUGATED FOIL rn December 1962 No. 1889 CD This Report is One of a Series Issued in

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:: Abstract Design curves are presented for determining the axial buckling stress of sandwich cylinders

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:: have been used in many previous analyses and are known to represent usual sandwich construction having

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:: of Long Cylinders of Sandwich Construction under Uni- form External Lateral Pressure, Nov. No. 1844

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:: compression is extended. Literal equations are derived that are used for the construction of design curves for

ScholarsArchive@OSU

Supplement no. 2 to stresses induced in a sandwich panel by load applied at an insert

Cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear

Compressive and shear properties of two configurations of sandwich cores of corrugated foil

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

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

Limit your search

Academic Affiliation

Advisor

Commencement Year

Conference Name

Creator

Date

Decade

Degree Field

Degree Level

Degree Name

File Format

Language

Non-Academic Affiliation

Peer Reviewed

Resource Type

Rights Statement

Subject

Search Constraints

Search Results

Limit your search