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Filtering by: Subject Magnesium alloys -- Testing File Format application/pdf Subject Aluminum alloys -- Testing

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 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
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