Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

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SCAN Goes Electronic! If you have electronic mail or if you can access the Internet, you can view biweekly issues of SCAN from your desktop absolutely free! Electronic SCAN takes advantage of computer technology to inform you of the latest worldwide, aerospace-related, scientific and technical information that has been published. No more waiting while the paper copy is printed and mailed to you. You can view Electronic SCAN the same day it is released—up to 191 topics to browse at your leisure. When you locate a publication of interest, you can print the announcement. You can also go back to the Electronic SCAN home page and follow the ordering instructions to quickly receive the full document. Start your access to Electronic SCAN today. Over 1,000 announcements of new reports, books, conference proceedings, journal articles...and more—available to your computer every two weeks. ii For Internet access to E-SCAN, use any of the following addresses: http://www.sti.nasa.gov ftp.sti.nasa.gov gopher.sti.nasa.gov To receive a free subscription, send e-mail for complete information about the service first. Enter scan@sti.nasa.gov on the address line. Leave the subject and message areas blank and send. You will receive a reply in minutes. Then simply determine the SCAN topics you wish to receive and send a second e-mail to listserv@sti.nasa.gov. Leave the subject line blank and enter a subscribe command, denoting which topic you want and your name in the message area, formatted as follows: Subscribe SCAN–02–01 Jane Doe For additional information, e-mail a message to help@sti.nasa.gov. Phone: (301) 621-0390 Fax: (301) 621-0134 Write: NASA STI Help Desk NASA Center for AeroSpace Information 7121 Standard Drive Hanover, MD 21076-1320 Looking just for Aerospace Medicine and Biology reports? Although hard copy distribution has been discontinued, you can still receive these vital announcements through your E-SCAN subscription. Just Subscribe SCAN-AEROMED Jane Doe in the message area of your e-mail to listserv@sti.nasa.gov. ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ ÎÎÎÎÎÎÎÎÎÎÎÎ
Subject Divisions Table of Contents Document citations are grouped first by the following divisions. Select a division title to view the categorylevel Table of Contents. A. Aeronautics H. Physics B. Astronautics I. Social and Information Sciences C. Chemistry and Materials J. Space Sciences D. Engineering E. Geosciences F. Life Sciences K. General G. Mathematical and Computer Sciences Indexes Two indexes are available. You may use the find command under the tools menu while viewing the PDF file for direct match searching on any text string. You may also select either of the two indexes provided for searching on NASA Thesaurus subject terms and personal author names. Subject Term Index Personal Author Index Document Availability Select Availability Info for important information about NASA Scientific and Technical Information (STI) Program Office products and services, including registration with the NASA Center for AeroSpace Information (CASI) for access to the NASA CASI TRS (Technical Report Server), and availability and pricing information for cited documents.
Page 1 and 2: Scientific and Technical Aerospace
Page 3: Introduction Scientific and Technic
Page 7 and 8: ground equipment and systems. For a
Page 9 and 10: Subject Categories of the Division
Page 11 and 12: 48 Oceanography 139 Includes the ph
Page 13 and 14: 72 Atomic and Molecular Physics 191
Page 15 and 16: Document Availability Information T
Page 17 and 18: Avail: NASA Public Document Rooms.
Page 19 and 20: NASA CASI Price Tables — Effectiv
Page 21 and 22: ALABAMA AUBURN UNIV. AT MONTGOMERY
Page 23 and 24: ��
Page 25 and 26: 20000061433 Pisa Univ., Dipartiment
Page 27 and 28: English; 34th; 34th Thermophysics C
Page 29 and 30: ciency of the generated derivative
Page 31 and 32: 20000063509 NASA Glenn Research Cen
Page 33 and 34: 05 AIRCRAFT DESIGN, TESTING AND PER
Page 35 and 36: A long tradition of aerodynamic des
Page 37 and 38: sonic and transonic cases will be p
Page 39 and 40: 20000061449 British Aerospace Publi
Page 41 and 42: 20000064593 NASA Langley Research C
Page 43 and 44: performance required for a proposed
Page 45 and 46: ment cost and create better product
Page 47 and 48: tion (NPSS), is focused on the inte
Page 49 and 50: surface measurement techniques used
Page 51 and 52: with emphasis on the search for lin
Page 53 and 54: 20000063520 NASA Kennedy Space Cent
Page 55 and 56:
primary issues for it’s adaptatio
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Footage shows the night vertical ta
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20000067665 NASA Kennedy Space Cent
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necessary for ignition modeling, or
Page 63 and 64:
engine lifetime, and high power ope
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24 COMPOSITE MATERIALS ��
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ments. For the screening of liner m
Page 69 and 70:
formation of a neutral, fluorescent
Page 71 and 72:
20000065655 Ames Lab., IA USA Funda
Page 73 and 74:
This is a second Triennial Conferen
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of completely charged PSSNa solutio
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20000064100 NASA Langley Research C
Page 79 and 80:
Spacecraft in low Earth orbit (LEO)
Page 81 and 82:
Pressure gradients, i.e. pressure h
Page 83 and 84:
agreed that the NO(sub x) levels co
Page 85 and 86:
tectural approach to extending the
Page 87 and 88:
20000064078 Physics and Electronics
Page 89 and 90:
20000064925 Institute for Human Fac
Page 91 and 92:
Page 93 and 94:
20000062455 National Inst. of Stand
Page 95 and 96:
Added Analysis (Risk Reduction); 6)
Page 97 and 98:
shipboard electrical power generati
Page 99 and 100:
20000067664 Jet Propulsion Lab., Ca
Page 101 and 102:
other, The theoretical framework go
Page 103 and 104:
figures compare the lift and pitchi
Page 105 and 106:
ment phase demonstrate desired feat
Page 107 and 108:
esolution mode with resolving power
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to track 1% or 0.5% changes was hig
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20000067643 NASA Marshall Space Fli
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37 MECHANICAL ENGINEERING ��
Page 115 and 116:
solver based on overset grid techno
Page 117 and 118:
Page 119 and 120:
20000064621 Rensselaer Polytechnic
Page 121 and 122:
that for a specific example of a be
Page 123 and 124:
km x 1000 km). As with the nearly c
Page 125 and 126:
20000064527 Analytical Imaging and
Page 127 and 128:
20000064533 Austin State Univ., Dep
Page 129 and 130:
20000064539 California Univ., Inst.
Page 131 and 132:
Page 133 and 134:
in Yellowstone National Park. We ar
Page 135 and 136:
terns of community hysteresis based
Page 137 and 138:
Page 139 and 140:
tion model (DEM) fitting to the sca
Page 141 and 142:
The Carolina slate belt is a 10- to
Page 143 and 144:
20000063373 Los Alamos National Lab
Page 145 and 146:
20000064912 New Energy and Industri
Page 147 and 148:
and discusses the issues and resear
Page 149 and 150:
The objective of this study was to
Page 151 and 152:
distributions with engine test resu
Page 153 and 154:
7.6, while the 1926 events appear t
Page 155 and 156:
We investigate the compositional di
Page 157 and 158:
Flight Center, USA; Moore, T. E., N
Page 159 and 160:
This report presents the Applied Me
Page 161 and 162:
in Goa, India, by 3 - 4 days. Wind
Page 163 and 164:
51 LIFE SCIENCES (GENERAL) Includes
Page 165 and 166:
20000062717 Joint Inst. for Nuclear
Page 167 and 168:
Page 169 and 170:
during 50% (SD 4%) of the breathing
Page 171 and 172:
20000064711 Massachusetts Inst. of
Page 173 and 174:
The analysis of this smaller data s
Page 175 and 176:
vided a functional helmet mount. Th
Page 177 and 178:
61 COMPUTER PROGRAMMING AND SOFTWAR
Page 179 and 180:
The goal of multi-image classificat
Page 181 and 182:
20000063526 Defence Science and Tec
Page 183 and 184:
85 dB amplifier design evolved by o
Page 185 and 186:
20000064594 New Mexico Univ., Elect
Page 187 and 188:
20000064615 NASA Ames Research Cent
Page 189 and 190:
declarations with a pattern recogni
Page 191 and 192:
containing point where interpolatio
Page 193 and 194:
has his own responsibility, while t
Page 195 and 196:
the people, documents and projects
Page 197 and 198:
and experimental technology, many o
Page 199 and 200:
tems. In particular this applicatio
Page 201 and 202:
Over the past decade, high performa
Page 203 and 204:
expensive than a single analysis. I
Page 205 and 206:
20000064726 Carnegie-Mellon Univ.,
Page 207 and 208:
20000064099 Teledyne Brown Engineer
Page 209 and 210:
20000066597 Geophysical Observatory
Page 211 and 212:
20000065633 Institute TNO of Applie
Page 213 and 214:
important conclusion is that for su
Page 215 and 216:
est frame of the string. The modifi
Page 217 and 218:
isotopes. The method and program we
Page 219 and 220:
A detailed study is undertaken, usi
Page 221 and 222:
20000063497 Kaiser Electro-Optics,
Page 223 and 224:
delivers 60% of the x-ray flux from
Page 225 and 226:
76 SOLID-STATE PHYSICS ��
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20000064660 Abdus Salam Internation
Page 229 and 230:
Page 231 and 232:
20000064703 Institute of Atomic Ene
Page 233 and 234:
The BRST approach is applied to the
Page 235 and 236:
20000067671 Hampton Univ., VA USA A
Page 237 and 238:
82 DOCUMENTATION AND INFORMATION SC
Page 239 and 240:
ecoming almost too cumbersome to be
Page 241 and 242:
physical world. These are the two p
Page 243 and 244:
with WFPC2 data. Tests of HSTphot
Page 245 and 246:
A brief description is given of the
Page 247 and 248:
20000064070 NASA Ames Research Cent
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gas, show variations that have rema
Page 251 and 252:
egy, called Power In that would all
Page 253 and 254:
20000065631 NASA Kennedy Space Cent
Page 255 and 256:
20000064089 Smithsonian Astrophysic
Page 257 and 258:
A ABERRATION, 143, 198 ABRASION, 22
Page 259 and 260:
COMPRESSIBLE FLOW, 83 COMPRESSION L
Page 261 and 262:
FATIGUE (MATERIALS), 50, 93, 96 FAT
Page 263 and 264:
LASING, 90 LATE STARS, 224 LATITUDE
Page 265 and 266:
PATCH ANTENNAS, 74 PATHOLOGY, 98 PA
Page 267 and 268:
SPACE PLATFORMS, 38 SPACE PROBES, 2
Page 269 and 270:
WIND PROFILES, 137 WIND TUNNEL TEST
Page 271 and 272:
Brown, Andy, 38 Brown, April S., 20
Page 273 and 274:
Grosvenor, C. A., 70 Grosvenor, J.
Page 275 and 276:
Lu, Gui-Ying, 50 Lugg, Desmond J.,
Page 277 and 278:
Robertson, Tony, 39 Robinson, Jeffr
Page 279:
Warner, J. D., 63 Warren, James, 16
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Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

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