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Tests of cargo flooring N and P for aircraft

Creator:: Liska, J. A. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed March 1956.
Resource Type:: Technical Report
Full Text:: thick on the lower facing. The facings on floor P were of FS-lh magnesium alloy 0.090 inch thick on the

Tests of cargo flooring Pp and U for aircraft

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:: . The upper or wearing surface of floor Pp was FS-1A magnesium alloy 0.090 inch thick, and that of floor

Tests of extruded magnesium cargo flooring for aircraft

Creator:: Liska, J. A. and Forest Products Laboratory (U.S.)
Resource Type:: Technical Report
Full Text:: assembled from five configurations of magnesium alloy extrusions. Teets simulating loads applied in ser

Effect of surface treatment on the adhesive bonding properties of magnesium

Creator:: Forest Products Laboratory (U.S.) and Eickner, Herbert W.
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:: was controlled to be 0.50 ± 0.01 inch. AZ31-H24, formerly designated as FS1-1-124,magnesium alloy

Tests of cargo flooring R and S for aircraft

Creator:: Liska, J. A. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed January 1959. Original report issued June 1948.
Resource Type:: Technical Report
Full Text:: .--' _' The two floors tested, designated R and S / were aluminum-alloy floors having a flat sheet-aluminum

Tests of cargo flooring M for aircraft

Creator:: Yolton, L. A. and Forest Products Laboratory (U.S.)
Resource Type:: Technical Report
Full Text:: dimpled aluminum-alloy sheet. These two sheets were spot-welded to a dimpled-sheet base formed to

Tests of cargo flooring-L for aircraft

Creator:: Yolton, L. A. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed March 1956. Original report issued October 1946.
Resource Type:: Technical Report
Full Text:: earlier reportl. Floor L consists essentially of an aluminum alloy sheet formed to typical rounded

A study of methods for preparing clad 24S-T aluminum-alloy sheet surfaces for adhesive bonding : part III. effect of cleaning methods on resistance of bonded joints to salt-water spray

Creator:: Forest Products Laboratory (U.S.) and Eickner, Herbert 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 March 1956 and 1962. Original report issued December 1950.
Resource Type:: Technical Report
Full Text:: A STUDY OF METHODS FOR PREIPAVING CLAD 24S-T ALUMINUM-ALLOY SHEET

A study of methods for preparing clad 24S-T3 aluminum-alloy sheet surfaces for adhesive bonding

Creator:: Forest Products Laboratory (U.S.), Eickner, Herbert W., and Schowalter, W. E.
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:: A STUDY CF METHODS FOR !PREPARING CLAD 24S-T3 ALUMINUM-ALLOY SHEET

Tests of cargo flooring Nn and T for aircraft

Creator:: Liska, J. A. and Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed March 1956. Original report published October 1948.
Resource Type:: Technical Report
Full Text:: cotton duck honeycomb core and 24ST aluminum alloy facings. The only difference in construction is the

Basic shear strength properties of metal-bonding adhesives as determined by lap-joint stress formulas of volkersen and goland and reissner

Creator:: Forest Products Laboratory (U.S.) and Eickner, Herbert W.
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 1960. Original report dated August 1955.
Resource Type:: Technical Report
Full Text:: tests were made of lap-joint specimens of clad 75S-T6 aluminum alloy with various lengths of overlap and

Strength of aluminum lap joints at elevated temperatures (tests conducted immediately after the temperature was reached)

Creator:: Kuenzi, Edward W. and Forest Products Laboratory (U.S.)
Abstract:: This report is one of a series issued in cooperation with Air Force-Navy-Civil Subcommittee on Aircraft Design Criteria under the supervision of the Aircraft Committee of the Munitions Board. Information reviewed and reaffirmed May 1954 and 1962. This report was originally published December 1949.
Resource Type:: Technical Report
Full Text:: Report No. 1804. Specimens and Methods of Testing Plates of clad 243-T3 aluminum alloy 5 by 8 inches

Tensile strength at elevated temperature of glued joints between aluminum and end-grain balsa

Creator:: Eickner, Herbert W. 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:: GLUED JOINTS BETWEEN ALUMINUM AND END-GRAIN BALSA 1 — By HERBERT EICIaTER, Engineer Aluminum alloy

The shear, fatigue, bend, impact, and long-time-load strength properties of structural metal-to-metal adhesives in bonds to 24S-T3 aluminum alloy

Creator:: Forest Products Laboratory (U.S.) and Eickner, Herbert W.
Abstract:: Information reviewed and reaffirmed May 1959 and 1965. Report originally published June 1953.
Resource Type:: Technical Report
Full Text:: PROPERTIES CI STRUCTURAL METAL-IC-METAL ADHESIVES IN BONDS TO 24S-T3 ALUMINUM ALLOY Information Reviewed

ScholarsArchive@OSU

Tests of cargo flooring N and P for aircraft

Tests of cargo flooring Pp and U for aircraft

Tests of extruded magnesium cargo flooring for aircraft

Effect of surface treatment on the adhesive bonding properties of magnesium

Tests of cargo flooring R and S for aircraft

Tests of cargo flooring M for aircraft

Tests of cargo flooring-L for aircraft

A study of methods for preparing clad 24S-T aluminum-alloy sheet surfaces for adhesive bonding : part III. effect of cleaning methods on resistance of bonded joints to salt-water spray

A study of methods for preparing clad 24S-T3 aluminum-alloy sheet surfaces for adhesive bonding

Tests of cargo flooring Nn and T for aircraft

Basic shear strength properties of metal-bonding adhesives as determined by lap-joint stress formulas of volkersen and goland and reissner

Strength of aluminum lap joints at elevated temperatures (tests conducted immediately after the temperature was reached)

Tensile strength at elevated temperature of glued joints between aluminum and end-grain balsa

The shear, fatigue, bend, impact, and long-time-load strength properties of structural metal-to-metal adhesives in bonds to 24S-T3 aluminum alloy

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