Image for Estimation of the Initial Buckling Stress Under Uniaxial Compression of a Corrugated Sandwich Panel

Estimation of the Initial Buckling Stress Under Uniaxial Compression of a Corrugated Sandwich Panel - Amendment B

Part of the Aircraft Structures series
See all formats and editions

Read More
Available
£150.00
Add Line Customisation
Usually dispatched within 4 weeks
Add to List
Product Details
ESDU International PLC
1862465320 / 9781862465329
Loose-leaf
01/06/1954
United Kingdom
4 pages
210 x 300 mm
General (US: Trade)/Professional & Vocational Learn More