Application of particle image velocimetry under cryogenic conditions (Englisch)
- Neue Suche nach: Richard, H.
- Neue Suche nach: Becker, W.
- Neue Suche nach: Loose, S.
- Neue Suche nach: Thimm, M.
- Neue Suche nach: Bosbach, J.
- Neue Suche nach: Raffel, M.
- Neue Suche nach: Richard, H.
- Neue Suche nach: Becker, W.
- Neue Suche nach: Loose, S.
- Neue Suche nach: Thimm, M.
- Neue Suche nach: Bosbach, J.
- Neue Suche nach: Raffel, M.
In:
20th International Congress on Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03.
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393-398
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2003
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ISBN:
- Aufsatz (Konferenz) / Elektronische Ressource
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Titel:Application of particle image velocimetry under cryogenic conditions
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Beteiligte:Richard, H. ( Autor:in ) / Becker, W. ( Autor:in ) / Loose, S. ( Autor:in ) / Thimm, M. ( Autor:in ) / Bosbach, J. ( Autor:in ) / Raffel, M. ( Autor:in )
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Erschienen in:
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Verlag:
- Neue Suche nach: IEEE
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Erscheinungsdatum:01.01.2003
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Format / Umfang:395978 byte
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ISBN:
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DOI:
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Medientyp:Aufsatz (Konferenz)
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Format:Elektronische Ressource
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Sprache:Englisch
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Datenquelle:
Inhaltsverzeichnis Konferenzband
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
- 1
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The Development of a 3 Component PIV System for the NASA Ames 12-foot Pressure Wind TunnelHeineck, J. T. / Walker, S. M. Z. / Institute of Electrical and Electronics Engineers et al. | 2003
- 1
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The development of a 3C-PIV system for the 12-foot pressure tunnel at NASA Ames Research CenterHeineck, J.T. / Walker, S.M. / Yaste, D.M. et al. | 2003
- 2
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On the development of Doppler global velocimetry for cryogenic wind tunnelsWillert, C. / Stockhausen, G. / Klinner, J. / Beversdorff, M. / Quest, J. / Jansen, U. / Raffel, M. et al. | 2003
- 15
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Analyses of flow field structures around linear-type aerospike nozzles using LIF and PSPNiimi, T. / Mori, H. / Okabe, K. / Masai, Y. / Taniguchi, M. et al. | 2003
- 15
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Analysis of Flow Field Structures around Linear-type Aerospike Nozzles using LIF and PSPNiimi, T. / Mori, H. / Okabe, K. / Masai, Y. / Institute of Electrical and Electronics Engineers et al. | 2003
- 21
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Particle image velocimetry in the crossplane of a supersonic jet in subsonic compressible crossflowBeresh, S.J. / Henfling, J.F. / Erven, R.J. et al. | 2003
- 31
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Trailing vortex detection and quantitative evaluation of vortex characteristics by PIV techniqueAlbano, F. / De Gregorio, F. / Ragni, A. et al. | 2003
- 44
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Multi-window PIV for High-lift Measurements in EuroPIV-2Arnott, A. / Schneider, G. / Neitzke, K.-P. / Agocs, J. / Sammler, B. / Schroder, A. / Kompenhans, J. / Institute of Electrical and Electronics Engineers et al. | 2003
- 44
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Multi-window PIV for high-lift measurementsArnott, A. / Schneider, G. / Neitzke, K.-P. / Agocs, J. / Sammler, B. / Schroder, A. / Kompenhans, J. et al. | 2003
- 54
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Tests for vehicle aerodynamics in the cryogenic wind tunnel Cologne DNW-KKKBecker, W. / Rebstock, R. / Loose, S. / Richard, H. / Raffel, M. et al. | 2003
- 54
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PIV - Tests for Vehicle Aerodynamics in the Cryogenic Wind Tunnel Cologne KKKRebstock, R. / Becker, W. / Richard, H. / Raffel, M. / Loose, S. / Institute of Electrical and Electronics Engineers et al. | 2003
- 59
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A PIV study on the effect of pulsed-jet injection upstream of a Mach 2 shock wave/turbulent boundary layer interactionBueno, P. / Hou, Y. / Clemens, N. / Dolling, D. et al. | 2003
- 70
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Optimization of temperature-sensitive paint formulation for large-scale cryogenic wind tunnelsIijima, Y. / Egami, Y. / Nishizawa, A. / Asai, K. / Fey, U. / Engler, R.H. et al. | 2003
- 77
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Transition detection by temperature sensitive paint at cryogenic temperatures in the European Transonic Wind tunnel (ETW)Fey, U. / Engler, R.H. / Egami, Y. / Iijima, Y. / Asai, K. / Jansen, U. / Quest, J. et al. | 2003
- 89
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MOSAIC project - summary of phase one programAsai, K. / Okura, I. / Mizushima, H. et al. | 2003
- 95
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A model deformation method applied to PSP measurementsYves Le Sant, et al. | 2003
- 95
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A Method to Correct Effects of Model Deformation on PSP ImagesLe Sant, Y. / Institute of Electrical and Electronics Engineers et al. | 2003
- 105
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Optoelectronic vibration measurement systemSimonov, V.L. / Kuzin, A.V. et al. | 2003
- 110
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Model deformation measurement in ETW using the Moire techniquePallek, D. / Butefisch, K.A. / Quest, J. / Strudthoff, W. et al. | 2003
- 115
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Intelligent system for optoelectronic surface vibration testingSimonov, V.L. / Kuzin, A.V. et al. | 2003
- 118
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Inverse method using infrared thermography for surface temperature and heat flux measurementsReulet, P. / Nortershauser, D. / Millan, P. et al. | 2003
- 127
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Dual PIV systems for space-time correlations in hot jetsWernet, M.P. / John, W.T. / Bridges, J. et al. | 2003
- 136
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Temperature and Velocity Distributions in Laminar Hypersonic Flat-Plate FlowO Byrne, S. / Danehy, P. M. / Houwing, A. F. P. / Institute of Electrical and Electronics Engineers et al. | 2003
- 136
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Plif temperature and velocity distributions in laminar hypersonic flat-plate flowO'Byrne, S. / Danehy, P.M. / Houwing, A.F.P. et al. | 2003
- 148
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A new data acquisition system for high speed pressure scannersCoulton, D.G. / Lambourne, M.G. et al. | 2003
- 157
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Optical skin friction measurements in the short-duration Ludwieg tube facilitySchulein, E. et al. | 2003
- 169
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Oil-Film Interferometry Measurement of Skin Friction- Analysis Summary and Describtion of a MATLAB ProgramNaughton, J. W. / Robinson, J. / Institute of Electrical and Electronics Engineers et al. | 2003
- 169
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Oil-Film interferometry measurement of skin friction - analysis summary and description of Matlab programNaughton, J.W. / Robinson, J. / Durgesh, V. et al. | 2003
- 179
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Application of stereoscopic PIV to helicopter rotor blade tip vorticesKato, H. / Watanabe, S. / Kondo, N. / Saito, S. et al. | 2003
- 190
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Rapid technology assessment via unified deployment of global optical and virtual diagnosticsJordan, 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. et al. | 2003
- 202
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A joint computational fluid dynamics and experimental fluid dynamics programTyler, C. et al. | 2003
- 202
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A Joint Computational Fluid Dynamics and Experimental Fluid Dynamics Test ProgramTyler, C. / Institute of Electrical and Electronics Engineers et al. | 2003
- 214
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Experimental study on controlling wake vortex in water towing tankFeng Bao, / Vollmers, H. / Mattner, H. et al. | 2003
- 224
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Airborne shock response spectra analyzer based on FPGAChen De-Rong, / Li Xiang-Bin, et al. | 2003
- 224
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Airborne Shock Response Spectrum Analyzer Based on FPGAChen, D. / Lei, W. / Institute of Electrical and Electronics Engineers et al. | 2003
- 228
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A Recirculation Flow Studied by Three Colour Particle Image VelocimetryDe Ponte, S. / Malavasi, S. / Svelto, C. / Matteazzi, G. / Institute of Electrical and Electronics Engineers et al. | 2003
- 228
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A recirculating flow studied by three colour particle image velocimetryDe Ponte, S. / Malavasi, S. / Svelto, C. / Matteazzi, G. et al. | 2003
- 236
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The evolved 100 kHz PWM-CTAHicks, T.J. / Schwannecke, J.K. / Norconk, M.J. / Hellum, A.M. / Foss, J.F. et al. | 2003
- 242
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High brightness, ultra-narrow linewidth Hg source for diagnosticsMiles, R.B. / Zaidi, S. / Lipeng Qian, / Vasilyak, L. et al. | 2003
- 247
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Experimental investigation of shock/vortex interaction for slender canard configurations at supersonic speedLeopold, F. / Jagusinski, F. / Demeautis, C. et al. | 2003
- 247
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Experimental Investigations of Vortex Breakdown for Slender Canard Configurations at Supersonic SpeedLeopold, F. / Institute of Electrical and Electronics Engineers et al. | 2003
- 258
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The interaction of streamwise vortex with a shock waveZudov, V.N. / Shevchenko, A. / Tretyakov, P.K. et al. | 2003
- 268
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Vortex Investigations Over a Rolling Delta Wind Model in Transonic Flow by Stereo PIV MeasurementsSammler, B. / Schroder, A. / Arnott, A. / Otter, D. / Agocs, J. / Kompenhans, J. / Institute of Electrical and Electronics Engineers et al. | 2003
- 268
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Vortex investigation over a rolling delta wing model in transonic flow by stereo PIV measurementsSammler, B. / Schroder, A. / Arnott, A. / Otter, D. / Agocs, J. / Kompenhans, J. et al. | 2003
- 278
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Radial profiles of arcjet flow properties measured with laser-induced fluorescence of atomic nitrogenGrinstead, J.H. / Driver, D.M. / Raiche, G.A. et al. | 2003
- 278
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Radial Profiles of Arcjet Flow Properties Measured with Two Photon Laser-induced Fluorescence of Atomic NitrogenGrinstead, J. H. / Driver, D. M. / Raiche, G. A. / Institute of Electrical and Electronics Engineers et al. | 2003
- 287
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N2/O2/H2 Dual-pump CARS: Validation ExperimentsO Byrne, S. / Danehy, P. M. / Cutler, A. D. / Institute of Electrical and Electronics Engineers et al. | 2003
- 287
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N/sub 2//O/sub 2//H/sub 2/ dual-pump cars: validation experimentsO'Byrne, S. / Danehy, P.M. / Cutler, A.D. et al. | 2003
- 296
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Optical diagnostics and instrumentation for supercritical combustion studies in a LOX/H/sub 2/ rocket engine combustion chamberKlimenko, D.N. / Clauss, W. / Mayer, W. / Oschwald, M. / Smith, J.J. et al. | 2003
- 296
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Optical Diagnostics and Instrumentation for super-criticalCombustion Studies in a lox/h2 Rocket Engine Combustion ChamberKlimenko, D. N. / Clauss, W. / Oschwald, M. / Smith, J. / Mayer, W. / Institute of Electrical and Electronics Engineers et al. | 2003
- 304
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Flow velocity measurements in nitrogen plumes stimulated by REMPIDankert, C. / Mori, H. et al. | 2003
- 309
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Recent enhancements to the OSU burst mode laser and MHz rate imaging systemsThurow, B. / Jiang, N. / Samimy, M. / Lempert, W. / Switzer, G. / Goss, L. et al. | 2003
- 320
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Simultaneous determination of temperature and velocity flow fields by enhanced two-color PTV techniqueMikheev, A.V. / Zubtsov, V.M. et al. | 2003
- 328
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High speed digital wavefront sensing for aero-optics and flow diagnosticsTrolinger, J. et al. | 2003
- 339
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A new optical measurement method for local wall shear stress and its signal processing techniquesShirai, K. et al. | 2003
- 351
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Temperature sensitive paint (TSP) for heat transfer measurement in short duration wind tunnelsMosharov, V. / Orlov, A. / Radchenko, V. et al. | 2003
- 357
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Application of PSP in low pressure regimeMori, H. / Niimi, T. / Yoshida, M. / Kondo, M. / Oshima, Y. / Hirako, M. et al. | 2003
- 363
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Surface pressure distribution imaging at frame rates over 1 kHz using porous pressure-sensitive paintSakamura, Y. / Suzuki, T. / Matsumoto, M. et al. | 2003
- 372
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Development of next generation lifetime PSP imaging systemsWatkins, A.N. / Jordan, J.D. / Leighty, B.D. / Ingram, J.L. / Oglesby, D.M. et al. | 2003
- 383
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Advancement of 2D profile testing at high Reynolds number in the cryogenic wind tunnel CologneJunnai Zhai, / Rebstock, R. et al. | 2003
- 393
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Application of particle image velocimetry under cryogenic conditionsRichard, H. / Becker, W. / Loose, S. / Thimm, M. / Bosbach, J. / Raffel, M. et al. | 2003
- 399
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The new low speed wind tunnel of the TU BraunschweigMoller, T.J. / Ortmanns, J. / El Khalfaoui, M. / Radespiel, R. et al. | 2003
- 403
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Authors| 2003
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20th International Congress on Instrumentation in Aerospace Simulation Facilities (IEEE Cat. No.03CH37501)| 2003