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Polar analysis of beam-columns for aircraft

Creator:: Jones, Walter Richard
Abstract:: The analysis of a member carrying a combination of lateral and axial loads (a "beam-column") is a problem of frequent occurrence in aircraft structural design. This thesis presents the derivation and application of the Polar method, both analytical and graphical. The method was first suggested in Germany, several years later...
Resource Type:: Masters Thesis
Full Text:: in airplane wing beam design, and it is therefore of interest to present the solution of this

Ground observers' guide

Creator:: United States. Department of the Air Force
Abstract:: Gerald W. Williams Collection
Resource Type:: Book

Durability of low-density core materials and sandwich panels of the aircraft type as determined by laboratory tests and exposure to the weather

Creator:: Forest Products Laboratory (U.S.), Heebink, Bruce G., Kommers, William J., and Mohaupt, Alvin A.
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 March 1956. Original report issued July 1950.
Resource Type:: Technical Report
Full Text:: DURABILITY Of LOW-DENSITY CORE MATERIALS AND SANDWICH PANELS Of

Durability of low-density sandwich panels of the aircraft type as determined by laboratory tests and exposure to weather

Creator:: Forest Products Laboratory (U.S.), Setterholm, Vance C., Heebink, Bruce G., and Kuenzi, Edward W.
Abstract:: This report is one of a series issued in cooperation with the ANC-23 Panel on Sandwich Construction of the Departments of the Air Force, Navy, and Commerce
Resource Type:: Technical Report
Full Text:: TYPE AS DETERMINED UY LABORATORY TESTS AND EXPOSURE TO WEATIFIER October 1955 This Report is One of

Durability of low-density core materials and sandwich panels of the aircraft type as determined by laboratory tests and exposure to the weather

Creator:: Forest Products Laboratory (U.S.), Heebink, Bruce G., Kommers, William J., and Kunzweiler, John J.
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:: DURABILITY OF LOW-DENSITY CORE MATERIALS AND SANDWICH PANELS Of

A photo-elastic analysis of an airplane gusset plate

Creator:: Johnston, Frederick Walter
Resource Type:: Masters Thesis
Full Text:: vlues of shear7 and 7axmay be found by a graphIcal construction tno'zm as Mohr's circle. The tormTmis

The effect of the forming properties of aluminum alloy 75S on aircraft construction

Creator:: Berlin, Edgar David
Resource Type:: Masters Thesis
Full Text:: into new production methods and tool design. The object of this paper is to draw together some of

Gluing wood in aircraft manufacture

Creator:: Truax, T. R. (Thomas Roy), 1886-
Resource Type:: Technical Report
Full Text:: assembly 4 820 Principles of cross-banded and laminated 20 wood construction 4 9 20 Cross-banded

The design of airplane wing ribs

Creator:: Newlin, J. A. (John A.), 1872-1943, Trayer, George W. (George William), 1888-1976, and Forest Products Laboratory (U.S.)
Abstract:: Reprint from National Advisory Committee for Aeronautics report 345. This report is one of a series issued to aid the nation's defense effort.
Resource Type:: Technical Report
Full Text:: the University of Wisconsin • THE DESIGN OF AIRPLANE WING RIBS * By J. A. NEWLIN and GEORGE W

Aircraft woods : their properties, selection, and characteristics

Creator:: Forest Products Laboratory (U.S.) and Markwardt, L. J. (Lorraine Joseph), 1889-
Abstract:: Reprint from National Advisory Committee for Aeronautics report 354. This report is one of a series issued to aid the nation's war program.
Resource Type:: Technical Report
Full Text:: material and workmanship, and error in the estimate of loads . STRenGTH VALUES FOR AIRCRAFT DESIGN Table

ScholarsArchive@OSU

Polar analysis of beam-columns for aircraft

Ground observers' guide

Durability of low-density core materials and sandwich panels of the aircraft type as determined by laboratory tests and exposure to the weather

Durability of low-density sandwich panels of the aircraft type as determined by laboratory tests and exposure to weather

Durability of low-density core materials and sandwich panels of the aircraft type as determined by laboratory tests and exposure to the weather

A photo-elastic analysis of an airplane gusset plate

The effect of the forming properties of aluminum alloy 75S on aircraft construction

Gluing wood in aircraft manufacture

The design of airplane wing ribs

Aircraft woods : their properties, selection, and characteristics

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