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Issue 10 Volume 41 May 16, 2003

Issue 10 Volume 41 May 16, 2003

Issue 10 Volume 41 May 16, 2003

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edge of the hole. The results of the analyses show that the predicted initial crack lengths compared well with the experimental<br />

measurements.<br />

DTIC<br />

Cracks; Crack Propagation; Solid Propellants; Strain Rate; Holes (Mechanics); Structural Analysis<br />

<strong>2003</strong>0032977 Brookhaven National Lab., Upton, NY<br />

Creating an ‘Electromagnetic Interference Risk Distribution Map’ In the Modern Hospital<br />

Spyropoulos, B.; Glotsos, D.; Batistatos, D.; Marneris, I.; Oct 2001; 5 pp.; In English; Original contains color illustrations<br />

Report No.(s): AD-A4<strong>10</strong>469; No Copyright; Avail: CASI; A01, Hardcopy<br />

Electromagnetic Interference (EMI) from various sources can cause medical monitoring equipment and other hospital<br />

devices to malfunction, that can range from mere inconvenience to serious problems. Comprehensive induced Magnetic Field<br />

and Real Electromotive Force measurements have been carried out and properly documented in the form of an ‘on line risk<br />

distribution map’ covering all departments in the General District Anti-Cancer Hospital of Piraeus ‘Metaxa’.<br />

DTIC<br />

Electromagnetic Interference; Medical Equipment<br />

<strong>2003</strong>0033000 Air Force Research Lab., Edwards AFB, CA, USA<br />

The Effects of Pressure on Fracture of a Rubbery Particulate Composite<br />

Miller, T. C.; Liu, C. T.; Jun. 2000; 18 pp.; In English<br />

Contract(s)/Grant(s): Proj-2302<br />

Report No.(s): AD-A4<strong>10</strong>517; AFRL-PR-ED-TP-2000-044; No Copyright; Avail: CASI; A03, Hardcopy<br />

There is a need for studying the effects of pressure on fractures. Recommendations for future work: examination of short<br />

crack fracture phenomena (why do short cracks behave differently?) Surface crack growth analysis: find a way to measure<br />

crack depth and width in pressurized environment. Links between microstructure and pressure effect (establish a connection<br />

between pressure effect and microstructural phenomena such as void nucleation, growth, and coalescence).<br />

DTIC<br />

Crack Propagation; Fracture Mechanics; Pressure Effects<br />

<strong>2003</strong>0033023 Virginia Polytechnic Inst. and State Univ., Blacksburg, VA<br />

Stress Intensity Factors and Paths for Cracks in Photoelastic Motor Grain Models Under Internal Pressure<br />

Smith, C. W.; Constantinescu, D. M.; Liu, C. T.; April 20, 2001; 11 pp.; In English<br />

Contract(s)/Grant(s): AF Proj. 2302<br />

Report No.(s): AD-A4<strong>10</strong>574; AFRL-PR-ED-TP-2001-<strong>10</strong>0; No Copyright; Avail: CASI; A03, Hardcopy<br />

Computational analysis and two-dimensional tensile tests on single motor grain fins suggest that cracks in fin tips are most<br />

likely to originate at the coalescence of a fin end tip radius, with a small radius from the side of the fin. Some manufacturers<br />

have also noticed defects formed during casting at the fin tip on the fin axis. The following is an experimental investigation<br />

utilizing frozen stress photoelastic models of an existing motor grain geometry in order to clarify stress intensity factor (SIF)<br />

values and crack growth paths for cracks emanating from the two above- noted potential critical loci. Comparisons between<br />

results from cracks grown from the two loci will be made, suggesting interesting conclusions.<br />

DTIC<br />

Crack Propagation; Rocket Engines; Internal Pressure; Stress Intensity Factors; Photoelasticity<br />

<strong>2003</strong>0034597 Air Force Research Lab., Edwards AFB, CA, USA<br />

Crack Growth Rates in a Propellant Under Various Conditions<br />

Miller, Tim; March 27, 2001; 18 pp.; In English<br />

Report No.(s): AD-A4<strong>10</strong>423; AFRL-PR-ED-VG-2001-053; No Copyright; Avail: CASI; A03, Hardcopy<br />

Cracks develop during manufacturing, handling and storage of rubbery particulate composites. During the service life, the<br />

cracks may begin to grow, but may still be subcritical because the cracks may grow slower than the burn rate of the propellant.<br />

Results for three types of specimens are described. This is done both at ambient and <strong>10</strong>00 psi (6895 kPa) pressure.<br />

DTIC<br />

Crack Propagation; Manufacturing; Pressure Dependence; Rocket Propellants<br />

188

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