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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:: CURVES FOR SANDWICH CYLINDERS HAVING ORTHOTROPIC FACINGS 1 — By CHARLES B. NORRIS, Engineer and JOHN

Creator:: Forest Products Laboratory (U.S.), Kommers, William J., and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: Information reviewed and reaffirmed 1962.
Resource Type:: Technical Report
Full Text:: compressive end load and the deflection under unifor m transverse Load . It is believed that a determination

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, Kommers, William J., and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed, October 1960. Original report dated October 1943.
Resource Type:: Technical Report
Full Text:: . KEIT1 dt and is a2 mi-nin+n m-i-n4. h n = 2 2Kh 1 / 1 n m + n k m n m ni Ewa, where a is

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, McKinnon, P. F., and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed, 1962. Original report published 1945.
Resource Type:: Technical Report
Full Text:: PILYWCIDID !PANELS el' SIZES MAT DO SICT PAULL 'WM TESTS M ►U AT VAPICUS ANCLIES TO THE FACE GRAIN TENSION

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, McKinnon, P. F., and Forest Products Laboratory (U.S.)
Abstract:: Publication restriction has been removed. Information reviewed and reaffirmed, 1962. Original report dated November 1943. 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:: face grain is parallel to the applied stress. Mimeo. No. 132g-A. -5- • • • • I ID0o....m g

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and McKinnon, P. F.
Abstract:: Information reviewed and reaffirmed, 1962. Original report published in 1946. 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:: not buckle. A partial verification 4 has been obtained for the case of tensile stresses by Lowell M

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and Kommers, William J.
Abstract:: Information reviewed and reaffirmed 1958. Original report issued June 1952.
Resource Type:: Technical Report
Full Text:: WITH A SHEAR LOAD By CHARLES B. NORRIS, Engineer and WILLIAM J. MIXERS, Engineer Forest Products

Creator:: Forest Products Laboratory (U.S.), Heebink, Bruce G., and Norris, Charles, B. (Charles Brazer), 1894-
Abstract:: Information reviewed and reaffirmed August 1961. This report was originally issued in February 1950.
Resource Type:: Technical Report
Full Text:: -4, •-• m: .1 4. -7 .44 -7 " -49 " "cam "4 '4 °' 1,14.341 r-kr,„1,11,48

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:: DISTRIBUTED NORMAL LOAD AND EDGEWISE, DIRECT? AND SBEAR LOADS-–. _ By CHARLES B. NORRIS, Engineer and

Creator:: Forest Products Laboratory (U.S.), Kuenzi, Edward W., and Norris, Charles, B. (Charles Brazer), 1894-
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. Information reviewed and reaffirmed March 1956 and 1962. Original report issued January 1948.
Resource Type:: Technical Report
Full Text:: g § 3 3i 8 2RR ?-1 2 R 2 § 8 3 N " "7, 821 M °A g N 710 E .?"4 .• HHHHHHHH H N HHHH N HHHH

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