Compression After Impact Experiments on Thin Face Sheet Honeycomb Core Sandwich Panels

Author:

McQuigg Thomas D.,Kapania Rakesh K.,Scotti Stephen J.,Walker Sandra P.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Reference13 articles.

1. TomblinJ.LacyT.SmithB.HooperS.VizziniA.LeeS. “Review of Damage Tolerance for Composite Sandwich Airframe Structures,” Federal Aviation Administration TR-DOT/FAA/AR-99/49, U.S. Dept. of Transportation, Office of Aviation Research, Aug. 1999.

2. “Composite Aircraft Structure,” Federal Aviation Administration Advisory Circular 20-107B, Change 1, U.S. Dept. of Transportation, Aug. 2010.

3. McQuiggT. “Compression After Impact Experiments and Analysis on Honeycomb Core Sandwich Panels with Thin Facesheets,” Ph.D. Dissertation, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, May 2011.

4. Impact Damage Resistance and Tolerance of Honeycomb Core Sandwich Panels

5. Barely Visible Impact Damage Evaluation of Composite Sandwich Structures

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