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Filtering by: Subject Barges -- Mathematical models Remove constraint Subject: Barges -- Mathematical models Creator Forest Products Laboratory (U.S.) Remove constraint Creator: Forest Products Laboratory (U.S.) Subject Sandwich construction -- Testing Remove constraint Subject: Sandwich construction -- Testing

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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:

cylinders having glass-fabric laminates of these types and honeycomb or isotropic cores. Mathematical
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
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:

Introduction Forest Products Laboratory Report No. 1871 (1) 3 presents two mathematical analyses 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:

II. NOTATION Page 1 4 III. MATHEMATICAL ANALYSIS (Rigorous Solution) 7 1. The Core
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
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:

. NOTATION 8 IV. MATHEMATICAL ANALYSIS 12 1. Determination of Displacement Functions which Satisfy
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:

orthotropic core. The core is assumed to be in a state of antiplane stress. The mathematical analysis employed
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

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Creator

Forest Products Laboratory (U.S.)[remove]31
Norris, Charles, B. (Charles Brazer), 1894 10
Kuenzi, Edward W.8
Raville, Milton E.4
Boller, Kenneth H.3
more Creators »

Date

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Current results range from 1953 to 1965

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1960-196916
1950-195915

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application/pdf31

Language

English [eng]31

Resource Type

Technical Report31

Rights Statement

Copyright Not Evaluated31

Subject

Sandwich construction -- Testing[remove]31
Buckling (Mechanics) -- Mathematical models15
Loads (Mechanics) -- Mathematical models6
Cylinders -- Testing5
Strains and stresses -- Mathematical models4
more Subjects »

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