Calculation of aircraft wing for static strength and stiffness
- Added: 23.06.2014
- Size: 723 KB
- Downloads: 0
Find out how to download this material
Subscribe to receive an information about new materials:
Description
There are no drawings.
Content 1 Preparation of initial information for strength calculation 1 1 Construction of ICAO diagram 1 2 Distribution of aerodynamic load by wing span 1 3 Distribution of inertial forces by wing span 1 4 Calculation of linear loads 1 5 Distribution of loads by wing chord 2 Construction of periods of forces and moments along the wing 2 1 Construction of epure of cutting forces and torques 2 2 Calculation of moments of the wing twist 3 Calculation of the wing 2
Content 1 Preparation of initial information for strength calculation 1 1 Construction of ICAO diagram 1 2 Distribution of aerodynamic load by wing span 1 3 Distribution of inertial forces by wing span 1 4 Calculation of linear loads 1 5 Distribution of loads by wing chord 2 Construction of periods of forces and moments along the wing 2 1 Construction of epure of cutting forces and torques 2 2 Calculation of moments of the wing twist 3 Calculation of the wing 2
Project's Content
|
Расчет крыла самолета на статическую прочность и жесткость.doc
|
Similar materials
Free downloading for today
Update after: 4 hours 33 minutes
