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Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on
Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on
召开年:
2003
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-
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1.
The development of a 3C-PIV system for the 12-foot pressure tunnel at NASA Ames Research Center
机译:
在NASA Ames研究中心为12英尺压力隧道开发3C-PIV系统
作者:
Heineck J.T.
;
Walker S.M.
;
Yaste D.M.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
wind tunnels;
drag reduction;
flow simulation;
aerospace testing;
flow measurement;
velocity measurement;
12-foot pressure tunnel;
NASA Ames research center;
three component particle image velocimetry system;
generic conventional model;
Reynolds number;
complex system design;
tractor-trailer model;
3.7 m;
2.
Intelligent system for optoelectronic surface vibration testing
机译:
光电表面振动测试智能系统
作者:
Simonov V.L.
;
Kuzin A.V.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
surface dynamics;
dynamic testing;
surface structure;
vibration measurement;
displacement measurement;
optical images;
measurement errors;
intelligent system;
optoelectronic surface vibration testing;
optoelectronic system;
complicated surface structure;
vibration measurement;
displacement measurement;
optical image;
errors compensation;
measurement errors;
mathematically model;
light functions;
3.
Optimization of temperature-sensitive paint formulation for large-scale cryogenic wind tunnels
机译:
大型低温风洞用热敏涂料配方的优化
作者:
Iijima Y.
;
Egami Y.
;
Nishizawa A.
;
Asai K.
;
Fey U.
;
Engler R.H.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
dyes;
stability;
polishing;
cryogenics;
optimisation;
wind tunnels;
luminescence;
boundary layers;
temperature sensors;
mean square error methods;
transonic flow;
optimization;
temperature sensitive paint system;
large scale transonic cryogenic wind tunnels;
boundary layer transition detection;
luminescence intensity;
robustness;
optimum dye binder solvent;
coating;
cryogenic temperatures;
root mean square roughness;
instability;
0.1 m;
4.
A recirculating flow studied by three colour particle image velocimetry
机译:
三色粒子图像测速研究循环流
作者:
De Ponte S.
;
Malavasi S.
;
Svelto C.
;
Matteazzi G.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
flow measurement;
velocity measurement;
image colour analysis;
aerodynamics;
computational fluid dynamics;
channel flow;
upstream recirculation flow;
downstream recirculation flow;
colour particle image velocimetry;
colour flashes;
water flow study;
water tunnel simulation;
aerodynamic phenomena;
cross correlation algorithm;
uniform distribution;
velocity measurement;
5.
Optical diagnostics and instrumentation for supercritical combustion studies in a LOX/H/sub 2/ rocket engine combustion chamber
机译:
用于LOX / H / sub 2 /火箭发动机燃烧室中超临界燃烧研究的光学诊断和仪器
作者:
Klimenko
;
D.N.
;
Clauss
;
W.
;
Mayer
;
W.
;
Oschwald
;
M.
;
Smith
;
J.J.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
oxygen;
hydrogen;
rocket engines;
combustion;
aerospace test facilities;
flow visualisation;
optical diagnostics;
optical instrumentation;
supercritical combustion;
H/sub 2/ rocket engine;
combustion chamber;
liquid oxygen;
hydrogen;
spray flames;
vehicle engines;
precise control;
combustor;
H/sub 2/;
O;
6.
Simultaneous determination of temperature and velocity flow fields by enhanced two-color PTV technique
机译:
增强型双色PTV技术同时测定温度和速度流场
作者:
Mikheev A.V.
;
Zubtsov V.M.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
drops;
flow measurement;
velocity measurement;
temperature measurement;
flow simulation;
computational fluid dynamics;
error analysis;
temperature flow field measurement;
velocity flow field measurement;
two color particle tracking velocimetry;
laser induced irradiation;
solid-liquid tracer particles;
radiation intensity;
CCD sensor;
error analysis;
measurement system;
calibration;
subpixel spatial resolution;
flow simulation;
computational fluid dynamics;
7.
A new data acquisition system for high speed pressure scanners
机译:
用于高速压力扫描仪的新型数据采集系统
作者:
Coulton D.G.
;
Lambourne M.G.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
data acquisition;
aircraft instrumentation;
pressure measurement;
aircraft testing;
data acquisition system;
high speed pressure scanners;
aircraft research association;
instrumentation/control systems;
data monitoring system;
high speed electronic scanners;
8.
Dual PIV systems for space-time correlations in hot jets
机译:
双PIV系统用于热喷时空关联
作者:
Wernet M.P.
;
John W.T.
;
Bridges J.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
flow measurement;
Mach number;
turbulence;
jets;
aeroacoustics;
convection;
dual PIV systems;
space time correlations;
hot jets;
digital particle image velocimetry;
DPIV system;
NASA;
national aeronautics and space administration;
gleen research center;
turbulence;
jet flows;
acoustic properties;
small hot jet acoustic rig;
Mach number;
independent traverse systems;
image acquisition;
time delays;
DPIV data;
first order flow properties;
cold jets;
convection;
mean axial velocity component;
turbulent kinetic energy;
cold flows;
hot flows;
jet axis;
phase delayed DPIV vector maps;
spatially separated DPIV vector maps;
9.
Inverse method using infrared thermography for surface temperature and heat flux measurements
机译:
使用红外热成像的逆方法进行表面温度和热通量测量
作者:
Reulet P.
;
Nortershauser D.
;
Millan P.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
laser beam effects;
temperature measurement;
infrared imaging;
discrete cosine transforms;
steel;
numerical analysis;
inverse method;
infrared thermography;
surface temperature measurement;
surface heat flux measurement;
surface heat flux identification;
boundary condition;
spatiotemporal variation estimation;
compression method;
DCT;
discrete cosine transform;
laser beam impact;
flat steel plate;
flame-wall interaction;
heat flux cartographies;
10.
N/sub 2//O/sub 2//H/sub 2/ dual-pump cars: validation experiments
机译:
N / sub 2 // O / sub 2 // H / sub 2 /双泵汽车:验证实验
作者:
OByrne
;
S.
;
Danehy
;
P.M.
;
Cutler
;
A.D.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
hydrogen;
nitrogen;
oxygen;
coherent antiStokes Raman scattering;
temperature measurement;
flames;
flow measurement;
optical pumping;
density measurement;
thermocouples;
computational fluid dynamics;
heat transfer;
dual pump CARS;
coherent antiStokes Raman spectroscopy;
temperature measurement;
RMS deviations;
root mean square deviations;
furnaces;
thermocouple measurements;
mean mole fraction;
standard deviation;
hydrogen air flat flame burner;
adiabatic equilibrium computation;
26 K;
64 K;
108 K;
300 to 1800 K;
N/sub 2/;
O/sub 2/;
H/sub 2/;
11.
Radial profiles of arcjet flow properties measured with laser-induced fluorescence of atomic nitrogen
机译:
激光诱导的原子氮荧光测量的电弧射流流动径向曲线
作者:
Grinstead J.H.
;
Driver D.M.
;
Raiche G.A.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
nitrogen;
density measurement;
temperature measurement;
velocity measurement;
fluorescence;
aerodynamics;
jets;
aerospace test facilities;
flow measurement;
arcjet flow properties;
laser induced fluorescence;
radial profile measurements;
atomic nitrogen density measurement;
velocity measurement;
temperature measurement;
aerodynamic heating facility test;
traversing system;
data analysis;
NASA Ames aerodynamic heating facility;
measurement uncertainties;
N;
12.
Surface pressure distribution imaging at frame rates over 1 kHz using porous pressure-sensitive paint
机译:
使用多孔压敏涂料以超过1 kHz的帧频对表面压力分布成像
作者:
Sakamura Y.
;
Suzuki T.
;
Matsumoto M.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
ruthenium;
porous materials;
silicon compounds;
gels;
paints;
pressure sensors;
pressure measurement;
jets;
shock waves;
nozzles;
flow measurement;
thin films;
surface pressure distribution imaging;
porous pressure sensitive paint;
unsteady flows;
dynamic response;
shock wave motion;
time resolved surface pressure measurements;
two dimensional Laval nozzle;
complementary metal oxide semiconductor;
CMOS camera;
bathophenanthroline ruthenium(II) complex;
silica gel thin layer chromatography aluminium plate;
step response;
frequency response;
pulse jet;
rapid flow evolution;
nozzle;
1 kHz;
Ru;
Al;
SiO/sub 2/;
13.
A model deformation method applied to PSP measurements
机译:
用于PSP测量的模型变形方法
作者:
Yves Le Sant
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
image processing;
cameras;
wind tunnels;
parameter estimation;
pressure measurement;
deformation;
deformation;
pressure sensitive paint measurements;
pressure sensitive paint images;
grid tracking;
marker tracking;
deformation law;
identification algorithm;
camera;
pressurized wind tunnel;
Onera Modane;
industrial wind tunnels;
parameter identification;
14.
Advancement of 2D profile testing at high Reynolds number in the cryogenic wind tunnel Cologne
机译:
低温风洞科隆中高雷诺数二维剖面测试的进展
作者:
Junnai Zhai
;
Rebstock R.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
aircraft testing;
laminar flow;
wind tunnels;
pressure measurement;
laser velocimetry;
boundary layers;
finite element analysis;
flow measurement;
aerodynamics;
infrared imaging;
flow simulation;
flow control;
2D profile testing;
Reynolds number;
cryogenic wind tunnel Cologne;
aircraft;
2D profile measuring technique;
wind tunnels;
servomotor;
synchronized motor drive system;
boundary layer control;
thermal load;
aerodynamic load;
motor drive system;
boundary conditions;
pressure measurement;
infrared thermograph;
laser velocimetry;
numerical methods;
wind tunnel wall effect;
wall correction method;
windmills;
laminar flow;
15.
Experimental study on controlling wake vortex in water towing tank
机译:
控制拖水罐尾流涡流的实验研究
作者:
Feng Bao
;
Vollmers H.
;
Mattner H.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
vortices;
wakes;
flow visualisation;
laser velocimetry;
flow control;
flow instability;
water towing tank;
self destructing vortex wake;
horizontal tail plains;
wing vortex sheet;
flow visualisation device;
tail vortices;
tip vortices;
self destructive mechanism;
instability;
wake vortex cores;
wing span;
transient process;
particle image velocimetry;
16.
Multi-window PIV for high-lift measurements
机译:
多窗口PIV用于高升程测量
作者:
Arnott A.
;
Schneider G.
;
Neitzke K.-P.
;
Agocs J.
;
Sammler B.
;
Schroder A.
;
Kompenhans J.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
wind tunnels;
wakes;
flow separation;
velocity measurement;
flow measurement;
flow simulation;
multiwindow PIV;
high lift measurements;
particle image velocimetry;
low speed wind tunnel;
two dimensional model;
slat model;
wing model;
flap model;
high lift configuration;
PIV data;
PIV image capture;
industrial wind tunnel tests;
slat wake;
wing wake;
slat gap;
wing gap;
flow separation;
17.
Oil-Film interferometry measurement of skin friction - analysis summary and description of Matlab program
机译:
油膜干涉法测量皮肤摩擦力-Matlab程序的分析摘要和说明
作者:
Naughton J.W.
;
Robinson J.
;
Durgesh V.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
friction;
liquid films;
flow control;
flow simulation;
aerodynamics;
flow measurement;
light interferometry;
computational fluid dynamics;
aerospace testing;
aerospace test facilities;
oil film interferometry;
skin friction measurement;
Matlab program;
wall shear stress measurement;
aerodynamic testing;
wall bounded flow;
computational simulations;
flow control;
interferograms;
18.
Particle image velocimetry in the crossplane of a supersonic jet in subsonic compressible crossflow
机译:
亚音速可压缩横流中超音速射流横切面的粒子图像测速
作者:
Beresh S.J.
;
Henfling J.F.
;
Erven R.J.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
supersonic flow;
subsonic flow;
compressible flow;
transonic flow;
aerodynamics;
jets;
motion measurement;
velocity measurement;
vortices;
wind tunnels;
particle image velocimetry instrument;
supersonic axisymmetric jet;
transonic wind tunnel;
subsonic compressible crossflow;
two dimensional measurement;
stereoscopic measurement;
counter rotating vortex;
streamwise plane data;
vortical motion measurement;
vertical velocity component;
19.
The interaction of streamwise vortex with a shock wave
机译:
流向涡与激波的相互作用
作者:
Zudov V.N.
;
Shevchenko A.
;
Tretyakov P.K.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
vortices;
shock waves;
Mach number;
flow visualisation;
subsonic flow;
jets;
Navier-Stokes equations;
flow simulation;
wakes;
streamwise vortex interaction;
plane shock wave interaction;
longitudinal vortex-normal shock interaction;
Mach numbers;
flow structure optical visualization;
Euler equations;
Navier-Stokes equations;
axisymmetric shock wave;
counterflow injection;
subsonic velocity;
gas jet parameters;
subsonic flow;
flow simulation;
wake;
20.
Vortex investigation over a rolling delta wing model in transonic flow by stereo PIV measurements
机译:
立体PIV测量在跨音速流中的三角翼模型上的涡旋研究
作者:
Sammler B.
;
Schroder A.
;
Arnott A.
;
Otter D.
;
Agocs J.
;
Kompenhans J.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
transonic flow;
vortices;
wind tunnels;
computational fluid dynamics;
flow simulation;
flow visualisation;
vortex investigation;
rolling delta wing model;
transonic flow;
particle image velocimetry measurements;
edge vortex;
cameras;
forward scatter mode;
light sheet thickness;
light sheet displacement;
optical system;
wind tunnel;
remote control;
optical tools;
trigger sequence;
optical fibres;
roll angle;
axial accelerations;
centrifugal accelerations;
pressure distributions;
CFD;
21.
A PIV study on the effect of pulsed-jet injection upstream of a Mach 2 shock wave/turbulent boundary layer interaction
机译:
对Mach 2冲击波/湍流边界层相互作用上游脉冲喷射注入影响的PIV研究
作者:
Bueno P.
;
Hou Y.
;
Clemens N.
;
Dolling D.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
jets;
vortices;
wind tunnels;
shock waves;
Mach number;
phase measurement;
velocity measurement;
boundary layer turbulence;
particle image velocimetry;
pulsed jet injection;
Mach 2 shock wave/turbulent boundary layer interaction;
upstream pulsed mass injection jets;
compresion ramp;
discrete pulsed underexpanded jets;
megapixel cameras;
unperturbed boundary layer;
phase locked PIV measurements;
injection trigger signal;
phase average PIV measurements;
bow shock upstream;
vortex generators;
momentum fluid;
upstream boundary layer;
60 mm;
5 m;
4 m;
22.
Application of stereoscopic PIV to helicopter rotor blade tip vortices
机译:
立体PIV在直升机旋翼桨叶涡旋中的应用
作者:
Kato H.
;
Watanabe S.
;
Kondo N.
;
Saito S.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
wind tunnels;
helicopters;
laser velocimetry;
vortices;
turbulence;
position measurement;
computational fluid dynamics;
velocity measurement;
rotors;
stereoscopic particle image velocimetry;
helicopter rotor blade tip vortices;
maximum blade vortex interaction noise;
low speed wind tunnel;
CCD cameras;
double pulse Nd:YAG laser;
azimuthal angles;
turbulence intensity;
vortex wander effects;
charge coupled device;
flowfields computation;
532 nm;
23.
Development of next generation lifetime PSP imaging systems
机译:
下一代终身PSP成像系统的开发
作者:
Watkins A.N.
;
Jordan J.D.
;
Leighty B.D.
;
Ingram J.L.
;
Oglesby D.M.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
paints;
CCD image sensors;
wind tunnels;
computational fluid dynamics;
pressure measurement;
temperature measurement;
flow measurement;
pressure sensitive paint imaging system;
LED lamps;
pulsed light emitting diode;
light transfer CCD camera;
charge coupled device;
noise sources;
calibration curves;
subsonic aerodynamic research laboratory;
Wright-Patterson air force base;
surface pressure distributions;
standard intensity based method;
lifetime imaging technique;
temperature measurement;
pressure measurement;
laser excitation source;
24.
Experimental investigation of shock/vortex interaction for slender canard configurations at supersonic speed
机译:
超音速细长鸭嘴结构的冲击/涡流相互作用的实验研究
作者:
Leopold F.
;
Jagusinski F.
;
Demeautis C.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
shock waves;
vortices;
supersonic flow;
flow visualisation;
wind turbines;
Mach number;
wind tunnels;
shock-vortex interaction;
slender canard configurations;
supersonic speed;
shock wave;
supersonic aircraft;
supersonic missiles;
supersonic vehicle;
streamwise wing tip vortices;
supersonic flows;
flow field visualizations;
laser Doppler velocimeter;
25.
High speed digital wavefront sensing for aero-optics and flow diagnostics
机译:
高速数字波前传感技术,用于航空光学和流量诊断
作者:
Trolinger J.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
wind tunnels;
flow measurement;
holographic interferometry;
image processing;
light interferometry;
optical images;
electro-optical devices;
high speed digital wavefront sensor;
aerooptics;
flow diagnostics;
dynamic wavefront sensing methods;
pumped solid state laser;
real time acquisition;
wind tunnel facilities;
electronic phase shifting interferometry methods;
flow field;
optical wavefront sensor;
optical imaging;
wavefront distortion;
wavefront correction;
electrooptics;
image processing;
robustness;
video recording;
interferometric wavefront;
holographic interferometry;
26.
Recent enhancements to the OSU burst mode laser and MHz rate imaging systems
机译:
OSU突发模式激光和MHz速率成像系统的最新增强功能
作者:
Thurow B.
;
Jiang N.
;
Samimy M.
;
Lempert W.
;
Switzer G.
;
Goss L.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
flow measurement;
optical parametric oscillators;
spectral line breadth;
laser modes;
solid lasers;
frame flow diagnostics;
OSU burst mode laser;
rate imaging systems;
Nd:YAG laser;
planar doppler velocimetry;
optical parametric oscillator;
burst mode pump;
spectral linewidth;
27.
A joint computational fluid dynamics and experimental fluid dynamics program
机译:
联合计算流体动力学和实验流体动力学程序
作者:
Tyler C.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
computational fluid dynamics;
velocity measurement;
wind tunnels;
aerodynamics;
flow measurement;
Mach number;
Doppler measurement;
force measurement;
light interferometry;
CFD;
computational fluid dynamics;
air vehicles;
lambda wing body aerodynamic configuration;
computational grid;
wind tunnel;
rapid prototyping;
force measurement;
moment measurement;
pressure sensitive paint;
projection Moire interferometry;
Doppler global velocimetry;
multiple trailing edge flap configuration;
Mach number;
subsonic aerodynamics;
nonintrusive measurement;
ground tests;
28.
A new optical measurement method for local wall shear stress and its signal processing techniques
机译:
局部壁面剪应力的新型光学测量方法及其信号处理技术
作者:
Shirai K.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
Doppler measurement;
signal processing;
time-frequency analysis;
flow simulation;
turbulence;
flow measurement;
optical variables measurement;
optical measurement method;
local wall shear stress;
signal processing techniques;
laser Doppler technique;
Doppler frequency;
Doppler burst signal;
spanwise offset;
scattering particle path;
time-frequency analysis;
nonlinear least squares fit;
simulated Doppler signals;
fluid flow simulation;
turbulence;
29.
Optical skin friction measurements in the short-duration Ludwieg tube facility
机译:
短期Ludwieg管设备中的光学皮肤摩擦测量
作者:
Schulein E.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
light interferometry;
wind tunnels;
liquid films;
friction;
computational fluid dynamics;
boundary layer turbulence;
flow simulation;
shock waves;
pipe flow;
optical skin friction measurements;
Ludwieg tube facility;
image acquisition;
image processing;
skin friction computations;
oil film interferometry technique;
shear stress distributions;
3D gradient flows;
three dimensional gradient flows;
short duration wind tunnel;
2D shock wave / turbulent boundary layer interaction flows;
two dimensional shock waves;
3D shock wave / turbulent boundary layer interaction flows;
30.
Plif temperature and velocity distributions in laminar hypersonic flat-plate flow
机译:
层流高超音速平板流动中的浆液温度和速度分布
作者:
OByrne S.
;
Danehy P.M.
;
Houwing A.F.P.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
hypersonic flow;
laminar flow;
velocity measurement;
temperature distribution;
boundary layers;
finite volume methods;
computational fluid dynamics;
flow measurement;
plif temperature distribution;
velocity distributions;
hypersonic laminar flat plate boundary layer;
rotational temperature;
planar laser induced fluorescence;
finite volume computation;
first order boundary layer computation;
edge displacement effects;
velocity measurement;
vibrational relaxation;
laminar flow;
hypersonic flat plate flow;
200 K;
31.
Rapid technology assessment via unified deployment of global optical and virtual diagnostics
机译:
通过统一部署全局光学和虚拟诊断程序进行快速技术评估
作者:
Jordan J.D.
;
Watkins A.N.
;
Fleming G.A.
;
Leighty B.D.
;
Schwartz R.J.
;
Ingram J.L.
;
Grinstead KD Jr.
;
Oglesby D.M.
;
Tyler C.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
wind tunnels;
interferometry;
data handling;
pressure sensors;
finite element analysis;
research and development;
computational fluid dynamics;
rapid technology assessment;
optical diagnostics;
virtual diagnostic interface;
air force research laboratory;
wright Patterson air force base;
Langley research center;
data translation methods;
low speed wind tunnel;
pressure distributions;
geometry measurements;
numerical simulations;
lifetime based pressure sensitive paint;
projection moire interferometry;
simulation based RD;
32.
Transition detection by temperature sensitive paint at cryogenic temperatures in the European Transonic Wind tunnel (ETW)
机译:
在欧洲跨音速风洞(ETW)中通过低温下的温度敏感涂料进行过渡检测
作者:
Fey U.
;
Engler R.H.
;
Egami Y.
;
Iijima Y.
;
Asai K.
;
Jansen U.
;
Quest J.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
dyes;
cryogenics;
laminar flow;
wind tunnels;
aerodynamics;
transonic flow;
infrared imaging;
data acquisition;
temperature measurement;
boundary layer turbulence;
laminar to turbulent transitions;
transition detection;
temperature sensitive paint;
cryogenic temperatures;
European transonic wind tunnel;
laminar turbulent boundary layer transition;
wing design;
flight Reynolds numbers;
cryogenic wind tunnels;
IR cameras;
infrared cameras;
cryogenic testing;
IR imaging;
data acquisition;
luminescent paint test;
temperature measurement;
33.
On the development of Doppler global velocimetry for cryogenic wind tunnels
机译:
低温风洞多普勒测速仪的发展
作者:
Willert C.
;
Stockhausen G.
;
Klinner J.
;
Beversdorff M.
;
Quest J.
;
Jansen U.
;
Raffel M.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
cryogenics;
wind tunnels;
Mach number;
laser velocimetry;
flow measurement;
Doppler measurement;
planar Doppler global velocimetry;
cryogenic wind tunnels;
Mach number;
gaseous nitrogen;
water vapor;
tunnel flow;
ice crystals;
nonintrusive measurement;
particle image velocimetry;
1.2 to 1.5 bar;
34.
Trailing vortex detection and quantitative evaluation of vortex characteristics by PIV technique
机译:
利用PIV技术进行尾涡检测和涡流特性定量评估
作者:
Albano F.
;
De Gregorio F.
;
Ragni A.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
aircraft;
wakes;
vortices;
data analysis;
data acquisition;
velocity measurement;
trailing vortex detection;
quantitative evaluation;
particle image velocimetry;
aircraft;
PIV measurements;
wake vortex;
data analysis;
PIV algorithms;
35.
Flow velocity measurements in nitrogen plumes stimulated by REMPI
机译:
REMPI激发的氮气羽流中的流速测量
作者:
Dankert C.
;
Mori H.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
nitrogen;
flow measurement;
nozzles;
supersonic flow;
velocity measurement;
flow velocity measurements;
nitrogen plumes;
REMPI;
resonance enhanced multiphoton ionization;
time of flight method;
TOF method;
electron beam bombardment;
laser beam;
angular velocity;
supersonic nozzles;
283 nm;
284 nm;
N/sub 2/;
36.
High brightness, ultra-narrow linewidth Hg source for diagnostics
机译:
高亮度,超窄线宽汞光源,用于诊断
作者:
Miles R.B.
;
Zaidi S.
;
Lipeng Qian
;
Vasilyak L.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
Rayleigh scattering;
Raman spectra;
mercury vapour lamps;
resonance;
spectral line breadth;
brightness;
flow measurement;
optical filters;
ultraviolet spectra;
Rayleigh scattering;
Raman scattering;
resonance enhancement;
ultra narrow linewidth radiation;
flow field diagnostics;
high efficiency mercury lamp;
mercury vapor filter;
mercury absorption cells;
9 kHz;
30 kV;
254 nm;
2 ns;
Hg;
37.
Model deformation measurement in ETW using the Moire technique
机译:
使用莫尔技术在ETW中进行模型变形测量
作者:
Pallek D.
;
Butefisch K.A.
;
Quest J.
;
Strudthoff W.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
deformation;
aircraft testing;
wind tunnels;
light interferometry;
model deformation measurement system;
Moire technique;
nonintrusive Moire interferometry system;
aircraft models deformation;
European transonic windtunnel;
wing twist;
wing bending;
evaluation software;
aircraft;
high Reynolds number tools and testing;
38.
Optoelectronic vibration measurement system
机译:
光电振动测量系统
作者:
Simonov V.L.
;
Kuzin A.V.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
vibration measurement;
dynamic testing;
measurement errors;
mathematical analysis;
optoelectronic system;
vibration measurement system;
oscillation measurement;
optical image;
mathematical modeling;
vibration testing;
aviation engine blades;
aviation turbine coolers;
printed circuit boards;
electronic devices;
acoustic loudspeakers;
optically active objects;
automotive industry;
distant measurements;
medical applications;
errors compensation;
climatic testing;
building block;
self testing;
39.
Tests for vehicle aerodynamics in the cryogenic wind tunnel Cologne DNW-KKK
机译:
低温风洞中的车辆空气动力学测试科隆DNW-KKK
作者:
Becker W.
;
Rebstock R.
;
Loose S.
;
Richard H.
;
Raffel M.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
aerodynamics;
cryogenics;
wind tunnels;
railways;
force measurement;
velocity measurement;
vehicle aerodynamics;
cryogenic wind tunnel Cologne;
aerodynamic design;
high speed trains;
particle image velocimetry test;
scaling factor;
contour ratios;
geometric ratios;
dutch wind tunnel;
40.
Analyses of flow field structures around linear-type aerospike nozzles using LIF and PSP
机译:
使用LIF和PSP分析线性气溶胶喷嘴周围的流场结构
作者:
Niimi T.
;
Mori H.
;
Okabe K.
;
Masai Y.
;
Taniguchi M.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
rocket engines;
flow visualisation;
pressure measurement;
space vehicles;
nitrogen compounds;
nozzles;
aerodynamics;
jet engines;
three dimensional flow field structures;
aerospike nozzles;
space shuttles;
rocket launch;
LIF;
laser induced fluorescence;
NO seeding;
N/sub 2/ gas;
pressure ratio;
vacuum chamber;
flow visualization;
pressure sensitive paint;
pressure measurement;
spike surface;
NO;
41.
Application of particle image velocimetry under cryogenic conditions
机译:
低温条件下颗粒图像测速仪的应用
作者:
Richard H.
;
Becker W.
;
Loose S.
;
Thimm M.
;
Bosbach J.
;
Raffel M.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
wind tunnels;
pressure measurement;
vortices;
flow measurement;
velocity measurement;
force measurement;
aerodynamics;
wakes;
aircraft testing;
laser velocimetry;
particle image velocimetry;
trailing vortices;
aircrafts;
wing tip devices;
cryogenic wind tunnel;
German-Dutch wind tunnels;
flow field measurements;
velocity field measurements;
force measurements;
moment measurements;
force measurement;
moment measurement;
pressure distribution measurements;
aerodynamic effects;
spatial vorticity distribution;
vortex strength;
wakes;
42.
Application of PSP in low pressure regime
机译:
PSP在低压领域的应用
作者:
Mori H.
;
Niimi T.
;
Yoshida M.
;
Kondo M.
;
Oshima Y.
;
Hirako M.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
ruthenium;
polymers;
paints;
photoluminescence;
pressure sensors;
pressure measurement;
Knudsen flow;
jets;
supersonic flow;
flow measurement;
pressure sensitive paint;
low pressure regime;
Knudsen number flows;
low density gas flows;
microflows;
anodized aluminum;
porphyrin complexes;
glassy polymer;
pressure distribution;
aluminum plate;
low density supersonic free jet;
pressure measurement;
luminescence;
150 Pa;
Ru;
Al;
43.
MOSAIC project - summary of phase one program
机译:
MOSAIC项目-第一阶段计划摘要
作者:
Asai K.
;
Okura I.
;
Mizushima H.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
research and development;
aerospace instrumentation;
aerodynamics;
thermodynamics;
chemical sensors;
pressure measurement;
temperature measurement;
molecular sensor for aerodynamic research;
phase one program;
interdisciplinary RD project;
Japanese science and technology agency;
optical sensing technology;
chemical molecules;
aerothermodynamic flow field;
electric sensors;
molecular sensor technology;
44.
Temperature sensitive paint (TSP) for heat transfer measurement in short duration wind tunnels
机译:
温度敏感涂料(TSP),用于短时风洞中的热传递测量
作者:
Mosharov V.
;
Orlov A.
;
Radchenko V.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
dyes;
paints;
heat transfer;
wind tunnels;
Mach number;
temperature measurement;
compressible flow;
flow measurement;
temperature sensitive paint;
heat transfer measurement;
surface heat transfer rates;
short-duration wind tunnel;
shock wind tunnels;
blunt nose cone model;
Mach number;
Ludwig scheme;
Reynolds numbers;
monochromatic colour;
two-color paint;
temperature insensitive dye;
light intensity variation;
heat flux;
40 ms;
45.
The evolved 100 kHz PWM-CTA
机译:
演进的100 kHz PWM-CTA
作者:
Hicks T.J.
;
Schwannecke J.K.
;
Norconk M.J.
;
Hellum A.M.
;
Foss J.F.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
pulse width modulation;
anemometers;
user interfaces;
computational fluid dynamics;
flow measurement;
channel flow;
pulse width modulation-constant temperature anemometer;
computer based user interface;
pulse width time resolution;
100 kHz;
46.
Airborne shock response spectra analyzer based on FPGA
机译:
基于FPGA的机载冲击响应谱分析仪
作者:
Chen De-Rong
;
Li Xiang-Bin
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
aerospace testing;
spectral analysers;
field programmable gate arrays;
space telemetry;
shock waves;
airborne shock response spectra analyzer;
FPGA;
field programmable gate arrays;
space vehicle telemetry;
three axis accelerometer;
flight test;
shock environment information;
limited system capacity;
shock data;
on board spectra;
47.
The new low speed wind tunnel of the TU Braunschweig
机译:
不伦瑞克工业大学的新型低速风洞
作者:
Moller T.J.
;
Ortmanns J.
;
El Khalfaoui M.
;
Radespiel R.
会议名称:
《Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on》
|
2003年
关键词:
wind tunnels;
jets;
heat exchangers;
flow measurement;
velocity measurement;
low speed wind tunnel;
fluid mechanics;
closed return atmospheric wind tunnel;
jet;
Reynolds number;
heat exchanger;
flow measurement instrumentation;
particle image velocimetry system;
test section;
flow constant;
140 m/s;
60 m/s;
0.8 m;
1.3 m;
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