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Filtering by: Alternative title ssim Technical note no. 205 Remove constraint Alternative title ssim: Technical note no. 205 Creator Forest Products Laboratory (U.S.) Remove constraint Creator: Forest Products Laboratory (U.S.) Subject Sandwich construction -- Testing Remove constraint Subject: Sandwich construction -- Testing

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Compressive and shear properties of two configurations of sandwich cores of corrugated foil

Creator:

Forest Products Laboratory (U.S.) and Stevens, Gordon H.

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:

SANDWICH CORES OF CORRUGATED FOIL rn December 1962 No. 1889 CD This Report is One of a Series Issued in
Effect of unbonded joints in an aluminum honeycomb-core material for sandwich constructions

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 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 May 1952.

Resource Type:

Technical Report

Full Text:

Technical Note 2152. Report No. 1835 -4- w = 0 . 04Thus t If the modulus of rigidity of the unbonded
Edgewise compressive strength of panels and flat wise flexural strength of strips of sandwich constructions

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:

53705 No. 1827 UNITED STATES DEPARTMENT OF AGRICULTURE FOREST SERVICE FOREST PRODUCTS LABORATORY
Elastic buckling of a simply supported rectangular sandwich panel subjected to combined edgewise bending and compression

Creator:

Forest Products Laboratory (U.S.) and Kimel, W. R.

Abstract:

Information reviewed and reaffirmed in 1962.

Resource Type:

Technical Report

Full Text:

Research Forest Products Laboratory Madison, Wisconsin 53705 No. 1857 `Sepiember-1-946. ""T4 REVIEWED
Repair of aircraft sandwich constructions

Creator:

Panek, Edward, Heebink, Bruce G., 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. Information reviewed and reaffirmed March 1956. Original publication dated May 1948.

Resource Type:

Technical Report

Full Text:

Laboratory Report No, 1574, June 1947. -Appendix I, Note 4, Report No. 1584 -2- The details of making
Aluminum facing and expanded-aluminum-honeycomb core sandwich material tested in shear

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:

- MUNITIONS I3CARD No. 1559- K Madison 5, Wisconsi n In Cooperation with the University of Wisconsi n
Aluminum face and paper honeycomb core sandwich material tested in shear

Creator:

Forest Products Laboratory (U.S.) and Werren, Fred

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:

the Supervision of the AERONAUTICAL DOARD ,No. 1559-A (ry rE0 ) UNITEDEATES 'DEPARTMENT OF
Tension test methods for wood, wood-base materials, and sandwich constructions

Creator:

Markwardt, L. J. (Lorraine Joseph), 1889-, Youngquist, W. G., and Forest Products Laboratory (U.S.)

Abstract:

Information reviewed and reaffirmed 1962. Original report issued June 1956.

Resource Type:

Technical Report

Full Text:

, Wisconsin 53705 No. 2055 June 1956 INFORMATION REVIEWED AND REAFFIRMED 1962 mu- 111 UNITED STATES
Cellular cellulose acetate core material with aluminum or fiberglas-laminate facings, tested in shear

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.

Resource Type:

Technical Report

Full Text:

resorcinol resin . Note 5. Adhesive V. A room temperature-setting resorcinol resi n Rept . No . 1559-F
Supplement to repair of aircraft sandwich constructions

Creator:

Forest Products Laboratory (U.S.), Mohaupt, Alvin A., and Heebink, Bruce G.

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:

area consisted of cutting holes at the end of the oval –Appendix, note 1. Report No, 1584 -A

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Creator

Forest Products Laboratory (U.S.)[remove]35
Werren, Fred6
Kuenzi, Edward W.5
Heebink, Bruce G.4
Norris, Charles, B. (Charles Brazer), 1894 4
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Date

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Current results range from 1947 to 1965

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Decade

1960-196913
1950-195917
1940-19495

File Format

application/pdf35

Language

English [eng]35

Resource Type

Technical Report35

Rights Statement

Copyright Not Evaluated35

Subject

Sandwich construction -- Testing[remove]35
Buckling (Mechanics) -- Mathematical models8
Shear (Mechanics)6
Honeycomb structures -- Testing5
Airframes -- Fatigue4
more Subjects »

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