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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:: 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

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

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

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

ScholarsArchive@OSU