Shear Buckling Analysis Of Honeycomb Sandwich Structure: Using FEA Software SAMCEF,Used

Shear Buckling Analysis Of Honeycomb Sandwich Structure: Using FEA Software SAMCEF,Used

Out of Stock
SKU: DADAX3838360834
Brand: LAP Lambert Academic Publishing
Condition: New
$95.65
Sold out
Free Standard Shipping Across USA
Quantity
Add to wishlist
Add to compare

Sold by Ergodebooks, an authorized reseller.

Returns accepted within 30 days | support@ergodebooks.com

Verified
Shipping Information
  • Free Standard Shipping — United States only
  • Processing Time: 3–5 business days
  • Estimated Delivery: 6–10 business days after dispatch
  • Double-boxed, fully insured & discreetly packaged
  • Tracking number sent via email once dispatched
Returns & Refund

Returns accepted within 30 days of delivery.

Damaged or Defective Item

Free return shipping + replacement or full refund

Wrong Item Received

Free return shipping + replacement or full refund

Change of Mind

Return shipping at customer's expense · 25% restocking fee applies

All returns require a Return Authorization (RA) number before sending.

To initiate a return, contact us:

support@ergodebooks.com +1 (281) 738-1050
View Full Return & Refund Policy
Payment Option
Payment Methods

Help

If you have any questions, you are always welcome to contact us. We'll get back to you as soon as possible, withing 24 hours on weekdays.

Customer service

All questions about your order, return and delivery must be sent to our customer service team by e-mail at yourstore@yourdomain.com

Sale & Press

If you are interested in selling our products, need more information about our brand or wish to make a collaboration, please contact us at press@yourdomain.com

Lighter and stiffer structural construction is required for space rockets than those used in aviation. A reduction of only 1 Kg in the weight of a rocket intended for a flight to Mars and back results in saving 2 tons of propellant. At present, sandwich technology is extensively used in Aeronautics and Aerospace fields. Sandwich panels with thin composite face sheets are used due to their ability to produce structures with high stiffness to weight and strength to weight ratios. In this research, Finite Element (FE) model is generated for a particular test configuration of honeycomb sandwich structure with metallic (Aluminium) skins. In this modelling effort, the specimen is modelled in such a way to simulate and analyze in a true sense. Stability and non linear analysis is carried out using FEA software SAMCEF. With geometric and material nonlinearity, the results are then compared with the experimental ones. Force displacement curves acquired from FEA and 3point bending test seem good enough for comparison.

⚠️ WARNING (California Proposition 65):

This product may contain chemicals known to the State of California to cause cancer, birth defects, or other reproductive harm.

For more information, please visit www.P65Warnings.ca.gov.

Recently Viewed