Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

More documents

Recommendations

Info

THERMAL PLASMAS, 135 THERMAL PROTECTION, 30 THERMAL STABILITY, 87 THERMOCHEMISTRY, 45 THERMODYNAMIC PROPERTIES, 52 THERMODYNAMICS, 48, 209 THERMOPHYSICAL PROPERTIES, 51 THIN FILMS, 63, 77 THIN PLATES, 190 THREE DIMENSIONAL FLOW, 41 THREE DIMENSIONAL MODELS, 4, 14, 23, 78, 97 THRUST, 79 TILES, 30 TIMBER IDENTIFICATION, 119 TIME DEPENDENCE, 11, 135, 233 TIME FUNCTIONS, 213 TIP SPEED, 188 TITAN, 228 TITAN 3 LAUNCH VEHICLE, 227, 230, 231 TITAN LAUNCH VEHICLES, 31 TITAN PROJECT, 228 TITANIUM, 43 TITANIUM ALLOYS, 52 TITANIUM ALUMINIDES, 52 TOPEX, 37 TOPOGRAPHY, 116 TORSION, 96 TOXICITY, 42, 143 TOXINS AND ANTITOXINS, 42 TRACKING (POSITION), 159, 190 TRAILING EDGES, 189 TRAINING ANALYSIS, 170, 171 TRAINING DEVICES, 170, 171, 214 TRAINING EVALUATION, 212, 214 TRAINING SIMULATORS, 27, 212 TRAJECTORIES, 9, 30 TRANSFER OF TRAINING, 60 TRANSFER ORBITS, 229 TRANSFERRED ELECTRON DEVICES, 73 TRANSFORMATIONS (MATHEMAT- ICS), 103, 109 TRANSIENT RESPONSE, 173 TRANSLATING, 157 TRANSMISSION LINES, 64, 71 TRANSONIC FLOW, 3, 15 TRANSPORT AIRCRAFT, 81 TRANSPORT PROPERTIES, 51 TRANSPORTATION, 33, 58 TRANSVERSE MOMENTUM, 193 TREES (PLANTS), 126 TREND ANALYSIS, 157 TRENDS, 127 TRIANGULATION, 131 ST–12 TRITIUM, 139 TROPICAL STORMS, 138 TROPOSPHERE, 125, 134, 135 TURBINE BLADES, 83 TURBINE PUMPS, 83 TURBINES, 41 TURBOFAN ENGINES, 23 TURBOFANS, 22 TURBOMACHINERY, 23 TURBULENCE, 188 TURBULENT BOUNDARY LAYER, 83, 191 TURBULENT FLOW, 4, 80, 83 TWINNING, 204 TWO DIMENSIONAL FLOW, 78 TWO DIMENSIONAL MODELS, 7, 14, 181 U U-2 AIRCRAFT, 116 ULTRAHIGH FREQUENCIES, 70 ULTRASONICS, 95 UNDERCARRIAGES, 20 UNDERWATER ACOUSTICS, 190, 191 UNIVERSITIES, 213 UNSTEADY STATE, 83 UNSTRUCTURED GRIDS (MATH- EMATICS), 156, 164 UPGRADING, 56 UPPER ATMOSPHERE, 135, 230 USER MANUALS (COMPUTER PRO- GRAMS), 17, 68, 216 V VACUUM, 55, 85 VACUUM CHAMBERS, 71 VACUUM EFFECTS, 53 VAPOR PHASES, 46 VARIABILITY, 232, 233 VARIABLE CYCLE ENGINES, 125 VARIABLE STARS, 223 VARIANCE (STATISTICS), 85 VARIATIONS, 198 VEGETATION, 100, 118 VEGETATIVE INDEX, 106, 113 VELOCITY MEASUREMENT, 202 VERTICAL FLIGHT, 35 VERTICAL LANDING, 35 VERTICAL TAKEOFF, 35 VERY LARGE SCALE INTEGRATION, 177 VIBRATION, 58 VIBRATION ISOLATORS, 58, 59, 93, 94 VIDEO COMMUNICATION, 217 VIDEO DISKS, 217 VIRTUAL MEMORY SYSTEMS, 174 VISCOUS FLOW, 181 VISCOUS FLUIDS, 78 VISIBILITY, 220 VISUAL ACUITY, 148 VISUAL CONTROL, 171 VISUAL OBSERVATION, 46 VOICE COMMUNICATION, 67 VOLATILITY, 151 VOLCANOES, 133 VOLCANOLOGY, 126, 132, 133 VOLUME, 213 VORTEX GENERATORS, 81 VORTICES, 189 VORTICITY, 41 VULNERABILITY, 65, 69 W WAFERS, 73, 76 WALLOPS ISLAND, 126 WALLS, 4 WARFARE, 69 WASTE ENERGY UTILIZATION, 122 WASTES, 45 WATER, 42, 123, 151 WATER DEPRIVATION, 144 WATER FLOW, 99 WATER IMMERSION, 145 WATER MANAGEMENT, 184 WATER QUALITY, 184 WATER RESOURCES, 99, 184 WATER RUNOFF, 104, 134 WATER SAMPLING, 126 WATERSHEDS, 104 WAVE DRAG, 3 WAVE FRONTS, 198 WAVE PROPAGATION, 17, 44 WAVE ROTORS, 25 WAVEGUIDE ANTENNAS, 64 WAVEGUIDES, 66, 190 WAVELENGTH DIVISION MULTI- PLEXING, 89 WAVELET ANALYSIS, 164 WEATHER, 214 WEATHER FORECASTING, 136, 137, 138 WEIGHT (MASS), 20 WEIGHT MEASUREMENT, 20 WEIGHTING FUNCTIONS, 59, 169 WELDED JOINTS, 95 WETLANDS, 126 WIDE AREA NETWORKS, 63 WILDLIFE, 181 WIND (METEOROLOGY), 137
WIND PROFILES, 137 WIND TUNNEL TESTS, 5, 17, 27 WIND VELOCITY, 139 WIND VELOCITY MEASUREMENT, 27 WING PLANFORMS, 3 WINGS, 14, 15 WORKLOADS (PSYCHOPHYSIOL- OGY), 8, 213 X X RAY BINARIES, 222 X RAY DIFFRACTION, 105, 201 X RAY IMAGERY, 232 X RAY OPTICS, 200 X RAY SOURCES, 201 X RAY SPECTRA, 222 X RAYS, 201, 232, 233 X-33 REUSABLE LAUNCH VEHICLE, 26, 215 X-34 REUSABLE LAUNCH VEHICLE, 215 X-38 CREW RETURN VEHICLE, 5, 215 XENON, 225 Y YELLOWSTONE NATIONAL PARK (ID-MT-WY), 111 YTTRIA-STABILIZED ZIRCONIA, 41 YTTRIUM OXIDES, 41 Z ZINC OXIDES, 206 ZONAL HARMONICS, 135 ST–13
Page 1 and 2:
Scientific and Technical Aerospace
Page 3 and 4:
Introduction Scientific and Technic
Page 5 and 6:
Subject Divisions Table of Contents
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
Page 57 and 58:
Footage shows the night vertical ta
Page 59 and 60:
20000067665 NASA Kennedy Space Cent
Page 61 and 62:
necessary for ignition modeling, or
Page 63 and 64:
engine lifetime, and high power ope
Page 65 and 66:
24 COMPOSITE MATERIALS ��
Page 67 and 68:
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
Page 75 and 76:
of completely charged PSSNa solutio
Page 77 and 78:
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
Page 109 and 110:
to track 1% or 0.5% changes was hig
Page 111 and 112:
20000067643 NASA Marshall Space Fli
Page 113 and 114:
37 MECHANICAL ENGINEERING ��
Page 115 and 116:
solver based on overset grid techno
Page 117 and 118:
20000067659 NASA Marshall Space Fli
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 ��
Page 227 and 228: 20000064660 Abdus Salam Internation
Page 229 and 230: 20000067648 NASA Marshall Space Fli
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
Page 249 and 250: 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: SPACE PLATFORMS, 38 SPACE PROBES, 2
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
show all

Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

Create successful ePaper yourself

Delete template?

Save as template?