Stress And Distortion Analysis Of A Swept Box Beam Having Bulkheads Perpendicular To The Spars


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Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars


Stress and Distortion Analysis of a Swept Box Beam Having Bulkheads Perpendicular to the Spars

Author: Richard R. Heldenfels

language: en

Publisher:

Release Date: 1950


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A method is presented for the approximate calculation of the stresses and distortions in a box beam representing the main structural component of a swept wing with a carry-through section and with bulkheads perpendicular to the spars. The application of the method is illustrated by a numerical example and its results are compared with previously published test data.

Technical Note - National Advisory Committee for Aeronautics


Technical Note - National Advisory Committee for Aeronautics

Author: United States. National Advisory Committee for Aeronautics

language: en

Publisher:

Release Date: 1950


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Annual Report of the National Advisory Committee for Aeronautics


Annual Report of the National Advisory Committee for Aeronautics

Author: United States. National Advisory Committee for Aeronautics

language: en

Publisher:

Release Date: 1950


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