Recommendations for Numerical Solution of Reinforced-Panel and Fuselage-Ring Problems / Nicholas J. Hoff, Paul A. Libby.

Format:

Book

Author/Creator:

Hoff, Nicholas J., author.

Libby, Paul A., author.

Series:

Report (United States. National Advisory Committee for Aeronautics) ; 934.

NACA Technical Report ; 934

Language:

English

Subjects (All):

Airplanes--Design and construction.

Airplanes.

Airplanes--Fuselage.

Physical Description:

1 online resource (29 pages) : illustrations.

Other Title:

Recommendations for Numerical Solution of Reinforced-Panel and Fuselage-Ring Problems

Place of Publication:

Washington, D.C. : National Advisory Committee for Aeronautics/NASA, 1949.

Summary:

Procedures are recommended for solving the equations of equilibrium of reinforced panels and isolated fuselage rings as represented by the external loads and the operations table established according to Southwell's method. From the solution of these equations the stress distribution can be easily determined. The method of systematic relaxations, the matrix-calculus method, and several other methods applicable in special cases are discussed. Definite recommendations are made for obtaining the solution of reinforced-panel problems which are generally designated as shear lag problems. The procedures recommended are demonstrated in the analysis of a number of panels. In the case of fuselage rings it is not possible to make definite recommendations for the solution of the equilibrium equations for all rings and loadings.

Notes:

Description based on publisher supplied metadata and other sources.

Includes bibliographical references.

ISBN:

1-68015-646-2