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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

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

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

Creator:: Forest Products Laboratory (U.S.) and Kimel, W. R.
Abstract:: Information reviewed and reaffirmed in 1962.
Resource Type:: Technical Report
Full Text:: approaches and data for sandwich structure design. It is known as the ANC-23 Panel. 1 The problem chosen

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

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

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

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:: Cooperation with the University of Wisconsin DESIGN CURVES FOR THE BUCKLING. OF SANDWICH CYLINDERS 1 OF

Creator:: Forest Products Laboratory (U.S.), March, H. W., and Kuenzi, Edward W.
Abstract:: Originally prepared and distributed in June 1953. Revised December 1957. Information reviewed and reaffirmed in 1965.
Resource Type:: Technical Report
Full Text:: CONSTRUCTION of the [Departments of the AIR FORCE, NAVY, ANC) COMMERCE BUCKLING OF SANDWICH CYLINDERS IN

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:: -23 PANEL ON SANDWICH CONSTRUCTION of the Departments of the AIR FORCE, NAVY, AND COMMERCE \'‘V,R A

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