Deformation analysis of wing structures
by Paul Kuhn
The elementary theories of bending and torsion often do not describe the stresses in aircraft shell structures with adequate accuracy; more refined stress theories have therefore have developed over a period of years. Theories of this nature are applied to the problem of calculating the deflections, particularly of wings. Bending as well as torsional deflections are discussed for wings without or with cut-outs. Whenever convenient, the formulas are given in such a form that they yield corrections to be added to the deflections calculated by means of the elementary theories. Examples show that the deflection corrections usually are quite small; very simple approximation formulas are therefore adequate for design purposes when conventional structures uder a reasonably uniform loading are being considered.
Check nearby libraries
Buy this book
Showing 1 featured edition. View all 1 editions?
| Edition | Availability |
|---|---|
1
Deformation analysis of wing structures
1947, National Advisory Committee for Aeronautics
in English
1680156071 9781680156072
|
aaaa
Libraries near you:
WorldCat
|
Book Details
Edition Notes
"Langley Memorial Aeronautical Laboratory."
Date of issue: July 1947.
Report no. NACA TN No. 1361.
Includes bibliographical references (page 34)
Classifications
The Physical Object
ID Numbers
Community Reviews (0)
Feedback?
| December 19, 2022 | Created by MARC Bot | import new book |