Determination of Honeycomb Material Properties: Existing Theories and an Alternative Dynamic Approach-Reference-Cited by-同舟云学术

Determination of Honeycomb Material Properties: Existing Theories and an Alternative Dynamic Approach

Published:2006-07 Issue:3 Volume:19 Page:177-183
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Schwingshackl C. W.¹²³,Aglietti G. S.¹²³,Cunningham P. R.¹²³

Affiliation:

1. Graduate Student, Astronautics Research Group, School of Engineering Sciences, Univ. of Southampton, Highfield, Southampton SO17 1BJ, U.K. (corresponding author).

2. Senior Lecturer in Aerospace Structural Dynamics, School of Engineering Sciences, Univ. of Southampton, Highfield, Southampton SO17 1BJ, U.K.

3. Principal Stress Engineer, Composites, Smith Aerospace Mechanical Systems-Aerostructures, Kings Av., Hamble-le-Rice, Southampton SO31 4NF, U.K.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282006%2919%3A3%28177%29

Reference31 articles.

1. The dynamic shear properties of structural honeycomb materials

2. ASTM. (1970). “C273 standard method of shear test in flatwise plane of flat sandwich constructions or sandwich cores.” ASTM C273 West Conshohocken Pa.

3. ASTM. (1988a). “C271 standard test method for density of core materials for structural sandwich constructions.” ASTM C271 West Conshohocken Pa.

4. ASTM. (1988b). “C365 standard test methods for flatwise compressive strength of sandwich cores.” ASTM C365 West Conshohocken Pa.

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