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

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

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

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

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

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

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

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

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:: , will lead to results that agree well with experiment. In the interest of simplicity, the mathematical

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, Kommers, William J., 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:: critical value. Discussion of Mathematical alis The deflections, bending moments, and shear loads of a

ScholarsArchive@OSU