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Design of composite sandwich panels for a Formula SAE monocoque chassis

Creator:: Story, Robert D.
Abstract:: Physical testing of composite sandwich panels in three point bending is an increasingly important aspect of qualifying a composite monocoque for Formula SAE competition. Required stiffness and strength values have increased over the past three years, and more of the monocoque's laminates must be tested as well. As a result,...
Resource Type:: Masters Thesis
Full Text:: Monocoque Chassis AN ABSTRACT OF THE THESIS OF Robert D. Story for the degree of Master of Science in

Supplement to the flexural rigidity of a rectangular strip of sandwich construction

Creator:: Norris, Charles, B. (Charles Brazer), 1894-, Ericksen, Wilhelm S., Kommers, William J., and Forest Products Laboratory (U.S.)
Abstract:: Supplementary mathematical analysis and comparison with the results of tests. 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:: SANDWICI1 CONSTRUCTION Supplementary Mathematical Analysis and Comparison with the Results of Tests

Flexural rigidity of a rectangular strip of sandwich construction

Creator:: Forest Products Laboratory (U.S.)
Abstract:: Information reviewed and reaffirmed September 1962. Original report dated February 1944.
Resource Type:: Technical Report
Full Text:: CONSTRUCTION Original report dated February 1944 Information Reviewed and Reaffirmed September 1962 No. 1505

Simply supported sandwich beam : a nonlinear theory

Creator:: Forest Products Laboratory (U.S.) and Zahn, John J.
Resource Type:: Technical Report
Full Text:: mathematical analysis are in the Appendix. Formula numbers ending in A refer to the appendix. 4—Underlined

Calculation of vibration damping in sandwich construction from damping properties of the cores and facings

Creator:: Forest Products Laboratory (U.S.) and James, William L.
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:: • CALCULATION OF VIBRATION DAMPING IN SANDWICH CONSTRUCTION FROM

Behavior of a rectangular sandwich panel under a uniform lateral load and compressive edge loads

Creator:: March, H. W. 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 1958. Original report issued September 1952.
Resource Type:: Technical Report
Full Text:: . Computationsfor the construction of curves for w were found to be simpler if values of E .were chosen to avoid

Design criteria for long curved panels of sandwich construction in axial compression

Creator:: Forest Products Laboratory (U.S.) and Kuenzi, Edward W.
Abstract:: This report is one of a series issued in cooperation with Army-Navy-Civil Committee on Aircraft Design Criteria under the supervision of the Aeronautical Board. Information reviewed and reaffirmed March 1956. Original report issued December 1946.
Resource Type:: Technical Report
Full Text:: of sandwich construction involves the possibilities of crimping (fig . 1) and wrinkling of the facin

An aeroelastic analysis of the Darrieus wind turbine

Creator:: Meyer, Edward Earnest
Abstract:: The stability of small oscillations of the troposkeinshaped blade used on Darrieus wind turbines is investigated. The blade is assumed to be attached to a perfectly rigid rotor shaft and spinning in still air. Linear equations of motion are derived which include the effects of in-plane, out-of-plane, and torsional stiffness,...
Resource Type:: Dissertation
Full Text:: the complex geometry of the Darrieus blades it was deemed necessary to use a computer model of the dy

Compressive buckling curves for sandwich cylinders having orthotropic facings

Creator:: Forest Products Laboratory (U.S.), Norris, Charles, B. (Charles Brazer), 1894-, and Zahn, John J.
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:: Cooperation with the ANC-23 PANEL ON COMPOSITE CONSTRUCTION FOR FLIGHT VEHICLES of the Departments of the AIR

Compressive buckling curves for flat sandwich panels with dissimilar facings

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 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:: Report Is One of a Series Issued in Cooperation with the ANC-23 PANEL ON COMPOSITE CONSTRUCTION FOR

ScholarsArchive@OSU

Design of composite sandwich panels for a Formula SAE monocoque chassis

Supplement to the flexural rigidity of a rectangular strip of sandwich construction

Flexural rigidity of a rectangular strip of sandwich construction

Simply supported sandwich beam : a nonlinear theory

Calculation of vibration damping in sandwich construction from damping properties of the cores and facings

Behavior of a rectangular sandwich panel under a uniform lateral load and compressive edge loads

Design criteria for long curved panels of sandwich construction in axial compression

An aeroelastic analysis of the Darrieus wind turbine

Compressive buckling curves for sandwich cylinders having orthotropic facings

Compressive buckling curves for flat sandwich panels with dissimilar facings

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