Fatigue of sandwich constructions for aircraft : Aluminum facing and expanded-aluminum-honeycomb core sandwich material tested in shear

An apparatus for measuring internal friction and fatigue strength of core materials used in sandwich construction

January 1965

This report is one of a series issued in cooperation with the ANC-23 panel on composite construction...

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

January 1958

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on ...

Elastic stability of the facings of flat sandwich panels when subjected to combined edgewise stresses

January 1960

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Fatigue of sandwich constructions for aircraft : Cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear

January 1962

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Fatigue of sandwich constructions for aircraft : Fiberglas-laminate facing and paper honeycomb core sandwich material tested in shear

February 1949

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Fatigue of sandwich constructions for aircraft : Glass-fabric-laminate facing and waffle-type core sandwich material tested in shear

October 1950

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Fatigue of sandwich constructions for aircraft : Fiberglas-honeycomb core material with fiberglas-laminate or aluminum facings, tested in shear

January 1962

Information reviewed and reaffirmed 1956 and 1962. Original report published 1948

Fatigue of sandwich constructions for aircraft : Cellular cellulose acetate core material with aluminum or fiberglas-laminate facings, tested in shear

December 1948

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Shear-fatigue properties of various sandwich construction

January 1965

Information reviewed and reaffirmed 1958 and 1965. Original report issued July 1952

Effect of unbonded joints in an aluminum honeycomb-core material for sandwich constructions

January 1958

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Stresses induced in a sandwich panel by load applied at an insert

January 1960

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Wrinkling of the facings of sandwich construction subjected to edgewise compression : sandwich constructions having honeycomb cores

June 1953

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Supplement to effects of shear deformation in the core of a flat rectangular sandwich panel : deflection under uniform load of sandwich panels having facings of moderate thickness

January 1958

This report is one of a series issued in cooperation with Air Force-Navy-Civil Subcomittee on aircra...

Repair of aircraft sandwich constructions

March 1956

This report is one of a series issued in cooperation with the Army-Navy-Civil Committee on aircraft ...

Mechanical properties of aluminum honeycomb cores

January 1962

This report is one of a series issued in cooperation with the ANC-23 panel on sandwich construction ...

An apparatus for measuring internal friction and fatigue strength of core materials used in sandwich construction

January 1965

This report is one of a series issued in cooperation with the ANC-23 panel on composite construction...

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

January 1958

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on ...

Elastic stability of the facings of flat sandwich panels when subjected to combined edgewise stresses

January 1960

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Fatigue of sandwich constructions for aircraft : Cellular-hard-rubber core material with aluminum or fiberglas-laminate facings, tested in shear

January 1962

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Fatigue of sandwich constructions for aircraft : Fiberglas-laminate facing and paper honeycomb core sandwich material tested in shear

February 1949

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Fatigue of sandwich constructions for aircraft : Glass-fabric-laminate facing and waffle-type core sandwich material tested in shear

October 1950

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Fatigue of sandwich constructions for aircraft : Fiberglas-honeycomb core material with fiberglas-laminate or aluminum facings, tested in shear

January 1962

Information reviewed and reaffirmed 1956 and 1962. Original report published 1948

Fatigue of sandwich constructions for aircraft : Cellular cellulose acetate core material with aluminum or fiberglas-laminate facings, tested in shear

December 1948

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Shear-fatigue properties of various sandwich construction

January 1965

Information reviewed and reaffirmed 1958 and 1965. Original report issued July 1952

Effect of unbonded joints in an aluminum honeycomb-core material for sandwich constructions

January 1958

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Stresses induced in a sandwich panel by load applied at an insert

January 1960

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Wrinkling of the facings of sandwich construction subjected to edgewise compression : sandwich constructions having honeycomb cores

June 1953

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Supplement to effects of shear deformation in the core of a flat rectangular sandwich panel : deflection under uniform load of sandwich panels having facings of moderate thickness

January 1958

This report is one of a series issued in cooperation with Air Force-Navy-Civil Subcomittee on aircra...

Repair of aircraft sandwich constructions

March 1956

This report is one of a series issued in cooperation with the Army-Navy-Civil Committee on aircraft ...

Mechanical properties of aluminum honeycomb cores

January 1962

This report is one of a series issued in cooperation with the ANC-23 panel on sandwich construction ...

An apparatus for measuring internal friction and fatigue strength of core materials used in sandwich construction

January 1965

This report is one of a series issued in cooperation with the ANC-23 panel on composite construction...

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

January 1958

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on ...

Elastic stability of the facings of flat sandwich panels when subjected to combined edgewise stresses

January 1960

This report is one of a series issued in cooperation with the Air Force-Navy-Civil Subcommittee on a...

Fatigue of sandwich constructions for aircraft : Aluminum facing and expanded-aluminum-honeycomb core sandwich material tested in shear

Abstract

Extracted data

Fatigue of sandwich constructions for aircraft : Aluminum facing and expanded-aluminum-honeycomb core sandwich material tested in shear

Abstract

Extracted data

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