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Residual strength properties of Gr/BMI composite laminates after constant/cyclic compression

Creator:: Shenoy, Krishnananda
Resource Type:: Masters Thesis
Full Text:: Strength Parameters 8 2.2 General Purpose Laminate Program - Gen lam 12 3. Component Material Properties

Adhesive bonding properties of various metals as affected by chemical and anodizing treatments of the surfaces (Part A - Additional tests on anodized aluminum and on zinc-chromate-primed magnesium)

Creator:: Forest Products Laboratory (U.S.) and Eickner, Herbert W.
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.
Resource Type:: Technical Report
Full Text:: the metal pieces. Testing The 3 lap-joint panels prepared with each metal, surface treatment, and

Adhesive bonding properties of various metals as affected by chemical and anodizing treatments of the surfaces

Creator:: Forest Products Laboratory (U.S.) and Eickner, Herbert W.
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. Revised April 1954. Addendum added. Supplement available with revisions. No. 1842A
Resource Type:: Technical Report
Full Text:: of 50 pounds per square inch. Testing Three of the lap-joint panels prepared with each bonding

Effect of elevated temperatures on the strengths of small specimens of sandwich construction of the aircraft type : tests conducted after exposure to elevated temperatures for 192 hours

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:: , "Fabrication of Lightweight Panels of the Aircraft Type." Testing Apparatus and Procedures Except for an

Effect of elevated temperatures on the strengths of small specimens of sandwich construction of the aircraft type : glass-cloth facings, balsa core -- tested immediately after the test temperature was reached

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:: of the aircraft type. Details as to testing apparatus and procedures were identical with those

Effect of elevated temperatures of the strengths of small specimens of sandwich construction of the aircraft type

Creator:: Forest Products Laboratory (U.S.) and Kuenzi, Edward W.
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 in August 1949.
Resource Type:: Technical Report
Full Text:: were conducted immediately after the speci- mens reached the desired temperature. Apparatus and testing

Development of a counterpart vertical fin of papreg for the AT-6 airplane

Creator:: Forest Products Laboratory (U.S.) and Jungmann, E. C.
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:: to the decision to investigate the utility of this material in a primary structural assembly in

Stress-rupture tests of a glass-fabric-base plastic laminate

Creator:: Boller, Kenneth H. 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. Information reviewed and reaffirmed 1959. Original report issued June 1953.
Resource Type:: Technical Report
Full Text:: tests are shown in table 1 and figure 4. In table 1 the strength values obtained by test in a testing

Shear-fatigue properties of various sandwich construction

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:: repeated shear stresses on the core material and on the bonds between the core and facings is therefore

An experimental approach to analyze large notched composite panels loaded in out-of-plane shear

Creator:: Froemming, Tyler M.
Abstract:: Identifying material characteristics of composites is important in designing any structural system. The aerospace industry relies on these material properties not only to design a functional aircraft, but also a safe and reliable one. Since carbon fiber composites are relatively new materials, little is known about its characteristics under certain...
Resource Type:: Masters Thesis
Full Text:: : _______________________________________________________________________ Brian K. Bay Identifying material characteristics of composites is important in

ScholarsArchive@OSU

Residual strength properties of Gr/BMI composite laminates after constant/cyclic compression

Adhesive bonding properties of various metals as affected by chemical and anodizing treatments of the surfaces (Part A - Additional tests on anodized aluminum and on zinc-chromate-primed magnesium)

Adhesive bonding properties of various metals as affected by chemical and anodizing treatments of the surfaces

Effect of elevated temperatures on the strengths of small specimens of sandwich construction of the aircraft type : tests conducted after exposure to elevated temperatures for 192 hours

Effect of elevated temperatures on the strengths of small specimens of sandwich construction of the aircraft type : glass-cloth facings, balsa core -- tested immediately after the test temperature was reached

Effect of elevated temperatures of the strengths of small specimens of sandwich construction of the aircraft type

Development of a counterpart vertical fin of papreg for the AT-6 airplane

Stress-rupture tests of a glass-fabric-base plastic laminate

Shear-fatigue properties of various sandwich construction

An experimental approach to analyze large notched composite panels loaded in out-of-plane shear

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