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ASTM Selected Technical Papers
Recent Advances in Composites in the United States and JapanAvailable to Purchase
By
JR Vinson
JR Vinson
1
University of Delaware
,
Newark, DE 19716
;
conference chairman and coeditor
.
Search for other works by this author on:
M Taya
M Taya
2
University of Delaware
,
Newark, DE 19716
;
conference secretary and coeditor
.
Search for other works by this author on:
ISBN-10:
0-8031-0436-7
ISBN:
978-0-8031-0436-5
No. of Pages:
739
Publisher:
ASTM International
Publication date:
1985

This project involved an experimental investigation into the effect of a high random acoustic loading, in combination with a static shear load near initial buckling, on the dynamic response of integrally stiffened graphite/epoxy panels. The program covered the design, fabrication, finite-element analysis, and testing of a J-stiffened monolithic panel and a J-stiffened minisandwich panel. The minisandwich panel had a syntactic core containing glass micro-balloons. The panels were designed to an initial shear buckling load of 17.51 kN/m (100 lb/in.). The predicted initial shear buckling load was, generally, in good agreement with the measured load. The damping, in all of the modes, increased significantly on approaching buckling. The root-mean-square strain, at the critical panel location, increased by as much as 30% in the vicinity of panel buckling, in spite of the increase in the damping.

1.
Soovere
,
J.
, “
The Effect of Acoustic-Thermal Environments on Advanced Composite Fuselage Panels
,” Paper Presented at the
24th Structures, Structural Dynamics and Materials Conference
,
Lake Tahoe, Nevada
, May 2–4, 1983.
2.
Jacobson
,
M. J.
, “
Sonic Fatigue of Advanced Composite Panels in Thermal Environments
,”
Journal of Aircraft
 0021-8669, Vol.
20
, No.
3
,
03
1983
.
3.
Soovere
,
J.
, “
Sonic Fatigue Testing of the NASA L-1011 Composite Aileron
,”
The Shock and Vibration Bulletin
, No.
4
, Part 4,
09
1980
.
4.
Soovere
,
J.
, “
Sonic Fatigue Testing of an Advanced Composite Aileron
,”
Journal of Aircraft
 0021-8669, Vol.
19
, No.
4
,
04
1982
.
5.
Ostrom
,
R. B.
, “
Post-Buckling Fatigue Behavior of Flat, Stiffened Graphite/Epoxy Panels Under Shear Loading
,”
Naval Air Development Center Report
No. NADC-78137-60,
05
1981
.
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