NASA Scientific and Technical Aerospace Reports
NASA Scientific and Technical Aerospace Reports
NASA Scientific and Technical Aerospace Reports
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designed to be the front-end of a haptic display system for virtual prototyping of assemblies.<br />
DTIC<br />
Polygons; Parameterization; Mathematical Models<br />
70<br />
PHYSICS (GENERAL)<br />
Includes general research topics related to mechanics, kinetics, magnetism, <strong>and</strong> electrodynamics. For specific areas of physics see<br />
categories 71 through 77. For related instrumentation see 35 Instrumentation <strong>and</strong> Photography; for geophysics, astrophysics, or solar<br />
physics see 46 Geophysics, 90 Astrophysics, or92 Solar Physics.<br />
20060001732 Tokyo Univ. of Agriculture <strong>and</strong> Technology, Japan<br />
Automatic Diagnosis of Pneumoconiosis by Texture Analysis of Chest X-Ray Images<br />
Kobatake, idefumi; Oh’ishi, Kunio; Miyamichi, Juichi; IEEE International Conference on Acoustics, Speech, <strong>and</strong> Signal<br />
Processing (ICASSP ‘87); Volume 1; 1987, pp. 14.16.1 - 14.16.4; In English; See also 20060001583<br />
Contract(s)/Grant(s): MOE-60302087; MOE-60550288; Copyright; Avail.: Other Sources<br />
This paper presents a study on automatic diagnosis of pneumoconiosis by texture analysis of chest X-ray images. A<br />
pre-processing method for normalizing distribution of film density is proposed <strong>and</strong> its effectiveness is studied experimentally.<br />
Dominant causes of the deviations of texture features for evaluating the profusion of small opacities are excluded by the<br />
pre-processing. New texture features based on the distribution of gradient vectors are also proposed. Experiments to evaluate<br />
the proposed system are demonstrated.<br />
Author<br />
Automatic Control; Diagnosis; Chest<br />
20060001787 Ball <strong>Aerospace</strong> <strong>and</strong> Technologies Corp., Albuquerque, NM USA<br />
Investigation of Burst Pressures Prediction of Slit Aluminum Cylinders Subjected to Localized Heating<br />
Sun, C. T.; Tanner, T.; Deitemeyer, A.; Nakaima, D.; Bruno, N.; Doering, D.; Tham, C.; Ulibarri, R.; Chen, J. K.; May 1, 2005;<br />
36 pp.; In English; Original contains color illustrations<br />
Contract(s)/Grant(s): F29601-00-D-0010-0014; Proj-ASCA<br />
Report No.(s): AD-A440210; AFRL-DE-PS-TR-2005-1095; No Copyright; Avail.: Defense <strong>Technical</strong> Information Center<br />
(DTIC)<br />
Crack Tip Opening Angle (CTOA) measurements of aluminum allow 2014-T6 (Al-2014-T6) at various temperatures <strong>and</strong><br />
the construction of the corresponding CTOA curves were performed. The CTOA curve as the crack growth criterion was used<br />
to simulate the burst pressures in Al-2014-T6 thin-walled cylinders with a longitudinal crack of different sized under thermal<br />
<strong>and</strong> mechanical load. The crack growth is simulated using nodal release method in the ABAQUS finite element environment<br />
to predict the burst pressure of axially cracked cylinders.<br />
DTIC<br />
Aluminum; Aluminum Alloys; Crack Propagation; Crack Tips; Heating; Slits<br />
20060001795 Army Research Lab., Adelphi, MD USA<br />
Feasibility Studies of New High Altitude Electromagnetic Pulse Test Materials<br />
Polun, Max; Nov. 1, 2005; 42 pp.; In English; Original contains color illustrations<br />
Report No.(s): AD-A440250; ARL-TR-3677; No Copyright; Avail.: Defense <strong>Technical</strong> Information Center (DTIC)<br />
The danger of a high-altitude electromagnetic pulse (HEMP) is one of many threats that an Army facility must be capable<br />
of surviving. A st<strong>and</strong>ard method of testing the HEMP survivability of these facilities exists. However. it is not capable of being<br />
used in all situations. This feasibility study used a series of experimental test methods <strong>and</strong> unique antenna designs to evaluate<br />
more flexible methods. The findings indicate that several of the antennae tested have suitable dynamic range characteristics<br />
<strong>and</strong> that alternative system designs can be employed where space limitations <strong>and</strong> other factors preclude use of the st<strong>and</strong>ard<br />
method.<br />
DTIC<br />
Electromagnetic Pulses; Feasibility; High Altitude; High Altitude Tests<br />
183