Accession Number:

AD0843804

Title:

Centaur Nose Fairing Honeycomb Specimen Test,

Personal Author(s):

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date:

1961-11-13

Abstract:

The purpose of the study was to determine Youngs modulus of the facing material, and the core shear modulus in bending of the sandwich structure as a function of core orientation and loading systems. Author

Pages:

0034

Descriptors:

Identifiers:

Subject Categories:

File Size:

0.00MB

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