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Creator:: Johnson, L. F. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed March 1956. Original report issued April 1949.
Resource Type:: Technical Report
Full Text:: Cooperation with the University of W;aconsin 111 TESTS OF CARGO FLOORING Pp AND U FOR AIRCRAFT By L. F

Creator:: Forest Products Laboratory (U.S.) and Werren, Fred
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 1958. Original report issued July 1952.
Resource Type:: Technical Report
Full Text:: e Sandwich Material " 1559-F "Cellular Cellulose Acetate Core Material with Aluminum or Fiberglas

Creator:: Werren, Fred 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.
Resource Type:: Technical Report
Full Text:: cycles o f approximately 64+ percent of the static strength for the condition of loadin g used

Creator:: Werren, Fred and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed 1958 and 1965. Original report issued July 1952.
Resource Type:: Technical Report
Full Text:: -facing bond. They are therefore considered to be indicative of the shear-fatigue properties that might be

Creator:: Forest Products Laboratory (U.S.) and Kuenzi, Edward W.
Abstract:: Information reviewed and reaffirmed 1958. Original report issued November 1951.
Resource Type:: Technical Report
Full Text:: • Tension - : Bond • 145 :Compression• • do • :. Tension • do • Sheet 5 of 6 Z M 87258 F Table 2

Creator:: Forest Products Laboratory (U.S.) and Kuenzi, Edward W.
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 1958. Original report issued April 1952.
Resource Type:: Technical Report
Full Text:: -grain balsa wood, at temperatures from 75° to 600° F. (23.9° to 315.6° C.). The experimental work

Creator:: Forest Products Laboratory (U.S.) and Kuenzi, Edward W.
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 1958.
Resource Type:: Technical Report
Full Text:: (160° to 600° F.) after exposure to those temperatures for 192 hours, and at room temperature after

Creator:: Forest Products Laboratory (U.S.), Heebink, Bruce G., Kuenzi, Edward W., and Ericksen, Wilhelm 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.
Resource Type:: Technical Report
Full Text:: : 171,17 ;Failure locations are shown by letters: C, core shear failure; B, bond failure; F, facing failure

Creator:: Forest Products Laboratory (U.S.) and Werren, Fred
Abstract:: Information reviewed and reaffirmed March 1956.
Resource Type:: Technical Report
Full Text:: Material" 1559-F "Cellular Cellulose Acetate Core Material with Aluminum or Fiberglas-laminate Facings

Creator:: Kuenzi, Edward W. and Forest Products Laboratory (U.S.)
Resource Type:: Technical Report
Full Text:: temperatures. The procedures employed have been found satis- factory for temperatures from 75° to 1,200° F

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