ICIASF '91 record Rockvolle, Maryland, USA, October 27 - 31, 1991

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Veröffentlicht: New York, NY Inst. of Electrical and Electronics Engineers 1991
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Datensatz im Suchindex

DE-BY-TUM_call_number 0001 92 B 748
DE-BY-TUM_katkey 575246
DE-BY-TUM_location Mag
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adam_text Table Of Contents Session 1 : Pressure Measurement Technology I Investigation on Optimizing the Design Process of 1 Multi-Hole Pressure Probes for Transonic Flow with Panel Methods T. Depolt and W. Koschel, Technical University of Aachen, Institute for Jet Propulsion and Turbomachinery A New Optical Pressure Measurement System 10 (OPMS) A. Vollan, Omega GmbH; and L. Alati, Inteco ari Aerodynamic Assessment of an Optical Pressure 17 Measurement System (OPMS) by Comparison with Conventional Pressure Measurements in a High Speed Wind Tunnel R.H. Engler and K. Hartmann, DLR, Göttingen; and B. Schulze, MBB A Probe for Measuring Pressure Fluctuations in 25 Flows M. Nasseri and W. Nitsche, Technische Universität Berlin Session 2: Optical Diagnostics An Optical Deflectometer for the Quantitative 34 Analysis of Turbulent Structures S.S. Mclntyre and G.S. Settles, Pennsylvania State University; and E. Stanewsky, DLR, Göttingen A New Look at Surface Flow Visualisation to 43 Provide Insight into Complex Fluid Dynamic Behavior R.G. DiMiccoand P.J. Disimule, University of Cin¬ cinnati Detecting 3-D, Turbulent Separation Regions 49 Using Unsteady Thermographie Technique R. Monti and G. Zuppardi, University of Naples Session 3; Flowfleld Measurements I Instabilities in the Near Wake of a Rod With an 60 Anchored Flame J. Quinard, Université de Provence, Centre St. Jérôme The Useof Silicon Microsensors in Smart Skins for 413 Aerodynamic Research D.L. Carraway, NASA Langley, Hampton Response of Turbulent Jet Flow to Rapid 68 Compression H J. Nuglisch, J. Borée, N. Atassi and G. Charnay, Institut de Méchanique des Fluides de Toulouse Nonintrusive Measurements in Fluid Dynamic 74 Flows from Mach .0005 to 14 G.L. Seibert, USAF, Wright-Patterson Air Force Base Session 4: Laser Doppier Velocimetry Techniques I A Machine Vision Particle Image Velocimetry 82 System for the Monitoring Opaque Slurry Motion I. Grant and Y.Y. Yan, Heríot-Watt University, Edinburgh DFLDA — A Miniaturized, Mobile Laser Doppler 85 Anemometer M. StieglmeierandC. Tropea, Universität Erlangen, Nürnberg Forced Convection in Joined Rectangular Grooves 94 Numerical Simulation of PIV and LDA Measurements A. Aroussi, Nottingham University; and I. Grant and Y.Y. Yan, Heriot-Watt University, Edinburgh Comparison of Frequency Domain and Time 103 Domain Laser Velocimeter Signal Processors J. Elliot, NASA Langley, Hampton; W.D. Mace, Jr., Lockheed, Hampton; and B. Blancha and J. Murphy, Macrodyne, Inc., New York Session 5 : Temperature Measurement Technology Notes on the Use of Fusible Temperature Indicators 113 to Bound the Temperature of Hot Graphite in the NAVSWC Hypervelocity Wind Tunnel Facility M.A. Metzger, NAVSWC, White Oak, Silver Spring, Maryland Correction Analysis for a Supersonic Water Cooled 123 Total Temperature Probe Tested to 1370 К N.T. Lagen, George Washington University, Hampton; and J.M. Seiner, NASA Langley, Hampton A Fine-Wire Thermocouple Probe for 136 Measurement of Stagnation Temperatures in Real Gas Hypersonic Flows of Nitrogen B.R. Hollis and W. Griffith, North Carolina State University; and W.J. Yanta, NAVSWC, White Oak, Silver Spring, Maryland A Laser-Induced Heat Flux Technique for 146 Convective Heat Transfer Measurement in High Speed Flows A.R. Porro and W.R. Hingst, NASA Lewis, Cleve¬ land; and T.G. Keith, University of Toledo Session 6: Infrared Imaging Session 9: Skin Friction Techniques Problems and Solutions for Transition Detection in 156 Cryogenic Wind Tunnels by Infrared Imaging E. Gartenberg, Old Dominion University, Norfolk; and R.E. Wright, Jr., NASA Langley, Hampton Infrared Surface Temperature Measurements in 169 NA VSWC s Hypervelocity Wind Tunnel No. 9 J. Lafferty and A.S. Collier, NAVSWC, White Oak, Silver Spring, Maryland Further Development of Infrared Technique for f Detection of Boundary Layer Transition in Wind Tunnel and Free Flight A. Quast, DLR, Braunschweig Quantitative Heat Transfer Measurements in 178 Hypersonic Wind Tunnels by Means of Infrared Thermography G. Simeonides, H.L. Boerringer, J. P. Vermeulen and J.F, Wendt, von Karman Institut for Fluid Dynamics, Rhode-Saint-Genése Session 7: Simulations A Research into Simulation and Test of Flight t Control System W. Jinzhong and J. Shuhui, Beijing University of Aeronautics and Astronautics Conception of a UHB-Engine Simulator for the 190 Essential Characteristics of a True Scale Engine H.T. Bolms and W. Bräunung, DLR, Göttingen Session 8: Wind Tunnel Calibration Recent Developments in Data Acquisition and 196 Control Systems at the Aircraft Research Association Limited D.G. Coulton, Aircraft Research Association Limited, Bedford Some Important Factors in Turbulence in Flight 206 Measurement Q. Chen, Technical University of Braunschweig A New System for Recording Unstable Aero- 214 dynamic Phenomena in NAVSWC Hypervelocity Wind Tunnel #9 S. Swmford. NAVSWC, White Oak, Silver Spring, Maryland Preliminary Airfoil Testing Experience in the NDA 223 Cryogenic Wind Tunnel Y. Yamaguchi, Y. Nakauchi, M. Yorozu and T. Saito, Motional Defense Academy Development of a Skin Friction Gauge for Use in an t Impulse Facility G. Kelly, J. Simmons and A. Pauli, University of Queensland Uncertainty Analysis on Thin-Oil-Film Skin 231 Friction Measurements in Compressible Flow J.P. Hubnerand B.F. Carroll, University of Florida Skin Friction Measurements in 3-D Boundary 442 Layers G. luso, M. Onorato and P. G. Stazzini, Politecnico di Torino Application of Biprism Shear Strain Ratemeter 240 in Two Dimensional Channel Flow H.J. Sun, Beijing Institute of Civil Engineering and Architecture Session 10: Spectroscopy/Photochemistry Technology A Laser Fluorescence Anemometer System for the 403 Langley 16 x 24 Water Tunnel F.K. Owen and G. Orngard, Compiere, Inc., Palo Alto; D. Neuhart, NASA Langley, Hampton Study of Rayleigh Scattering for Visualization 246 of Helium-Air Mixing at Mach 6 B. Shirinzadeh, R.J. Balla, M.E. Hillard, J.B. Anders and R.J. Exton, NASA Langley, Hampton; I.A. Waltz, California Institute of Technology Rayleigh Imaging and Flow Tagging in Ground 255 Test Facilities R.B. Miles, W.R. Lempert, B. Zhang, J. Forkey and I. Glesk, Princeton University Requirements for Temperature Measurements in 262 Nonequilibrium Flows Using Laser-Induced O2 Fluorescence J.H. Grinstead andG. Laufer, University of Virginia Session 11: Interferometry A Real-Time Line of Sight Interferometer Tested at t University of Queensland TQ Facility T. Posillioo and J. Tamagno, GASL; and A. Pauli, University of Queensland Optical Processing of Gabor Holograms for 3D f Simultaneous Velocity Measurements C.S. Moraltis, von Karman Institute for Fluid Dynamics, Rhode-Saint-Genése A Real Time Interferometry System for Unsteady 423 Flow Measurements N.J. Brock, Aerometrics, Sunnyvale; and M.S. Chandrasekhara and L.W . Carr, NASA Ames, Monterey Session 12: Hot-Wire/Film Technology Session 15: Ground Test Facilities A Hot Wire for Detecting Wall-Shear Stress 270 Direction S. De Ponte and M. Parrini. Dipartimento di Ingegneria Aerospaziale A Simple Three Component Velocity Measurement 277 Method Using a Rotated Split-Film Sensor L.S. Miller and K, Yano, The Wichita State University Shock Detection on Airfoils by Means of Piezo Foil 284 and Hot Film Arrays M. Swoboda, W. Nitsche and J. Suttan, Technische Universität Berlin Session 13: Pressure Measurement Technology II Development of Multi-Channel Cryogenic f Instrumentation for ETW Models R.G. Scurlook and R. Webb, University of Southampton Thermal Compensation of Semiconductor Strain 431 Gauge Type Pressure Transducers Using a Real- Time Process C.R. Pyne, Royal Aerospace Establishment, Bedford Data Correction for Pressure Transmission Lines 295 Using Discrete Time Series Models S.M. Batill and J.V. Nebres, University of Notre Dame Application of a Wall Pressure Method in a Wind 304 Tunnel Test Section with Adjustable Longitudinal Slots H. Hoist and A. Heddergott, DLR, Göttingen Automatic Control of Test Parameters for Intake 348 Measurements in a Low-Speed Wind-Tunnel R. Friedrichs and R. Siebert, DLR, Braunschweig The Wind Tunnel Test System of 1995; Cost 359 Effective Experimentation Through a Fusion of Related Technologies R.D. Neumann, Science Applications International Corporation, Ohio; L. Webster, TeSCO, inc., Tennessee Hypervelocity Wind Tunnel 9 Control System 372 D. Newell and S. Rinaldi, NSWC, White Oak, Silver Spring, Maryland A Unique and Simple Automatic Pressure Regula- t ting System for a Small Blow-Down Wind Tunnel M.A. Ramaswamy, S.S. Pai, M. Vasagam and B.R. Arun, Indian Institute of Science, Bangalore Evaluation of Electrolytic Tilt Sensors for Wind- 382 Tunnel Model Angle-of-Attack (AOA) Measurements D.T. Wong, NASA Langley, Hampton Session 16: Flowfleld Measurements II A Comparison of Techniques for the Determination t of Stagnation Location M.A. Scott, D.L. Carraway and C.C. Lee, NASA Langley, Hampton Fault Diagnostics on Jet Engine Starting 392 H.Z. Liu, H.M. Wang and X.Q. Ni, Beijing Univer¬ sity of Aeronautics and Astronautics Calibration Stand for a Multi-Thruster Cluster 397 M. Ringel and D. Levin, Technion, Haifa, Israel Session 14: Laser Doppler Velocimetry Techniques II Particle Image Velocimetry Measurements of the 314 Aerodynamics of a Wind Turbine 1. Grant, G.H. Smith and A. Liu, Heriot-Watt University, Edinburgh; D. Infield, Rutherford Appleton Laboratory, Didoot; and T. Eloh, University of Essen Signal Processing Schemes for Doppler Global 321 Velocimetry J.F. Meyers and J.W. Lee, NASA Langley, Hampton; må A.A. Gavone, Vigyan, Inc., Virginia Spectra Analysis with a LDA in High Speed Flows 329 P. Dupont, DLR, Göttingen Comparison of Laser Transit Anemometry Data 336 Analysis Techniques W.M. Humphreys and L.R. Gartrell, NASA Langley, Hampton Author Index Alati. L ................ 10 Anders. J.B ............. 246 Aroussi. A .............. 94 Atassi, N ............... 68 Balla. R.J ..............246 Baiili. S.T ..............295 Blancha. В ..............103 Boerrigter. H.L ...........178 Bolms, H.T .............190 Boree. J ............... 68 Braünling, W ............190 Brock, N.J ..............423 Carr. L.W .............. 423 Carraway. D.L ........... 413 Carroll, B.F ............. 231 Cavone. A.A ............ 321 Chandrasekhara, M.S ....... 423 Charnay, G ............. 68 Chen, Q ............... 206 Collier, A.S ............. 169 Coulton. D.G ............ 196 Depóit, T ................ 1 DePonte, S ..............270 DiMicco, R.G ............ 43 Disimilie, PJ ............ 43 Dupont, P ..............329 Eich, T................ 314 Elliott, J ...............103 Engler, R.H ............. 17 Exton, R.J ..............246 Forkey, J ...............255 Friedrichs, R............348 Gartenberg, E ............156 Gartrell, L.R............336 Glesk, 1 ................255 Grant, 1 ...........82, 94, 314 Griffith, W ..............136 Grinstead, J.H ............262 Hartmann, К ............ 17 Heddergott, А ............ 304 Hillard, M.E............. 246 Hingst, W.R............. 146 Hollis, B.R............. 136 Holst, H ............... 304 Hubner, J.P............. 231 Humphreys. W.M......... 336 Infield, D ..............314 Isuo. G ................442 Keith, T.G ..............146 Koschel, W .............. i Lafferty, J .............. 169 Lagen, N.T............. 123 Laufer, G .............. 262 Lee, J. W ............... 321 Lempert, W.R ............ 255 Levin, D ............... 397 Liu, A ................ 314 Liu, H.Z ............... 392 Mace, W.D., Jr........... 103 Mclntyre, S.S ............ 34 Metzger, M.A ............ 113 Meyers, J.F............. 321 Miles, R.B .............. 255 Miller, L.S.............. 277 Monti, R ............... 49 Murphy, J .............. 103 Nakauchi, Y .............223 Nasseri, M .............. 25 Nebres, J.V .............295 Neuhart, D.............. 403 Neumann, R.D ...........359 Newell, D ..............372 Ni, X.Q ...............392 Nitsche, W ........... 25, 284 Nuglísch, HJ ............ 68 Onorato, M .............442 Orngard, R ..............403 Owen, F.K..............403 Panini, M ..............270 Porro, A.R ..............146 Pyne, C.R ..............431 Qe, J.Y ................240 Quinard, J .............. 60 Rinaldi, S ..............372 Ringel, M ..............397 Saito, T ................ 223 Schulze, B .............. 17 Seibert, G.L............. 74 Seiner, J.M............. 123 Settles, G.S ............. 34 Shirinzadeh, B ........... 246 Siebert, R.............. 348 Simeonides, G ........... 178 Smith, G.H ............. 314 Stanewsky, E ............ 34 Stazzini, P.G ............ 442 Stieglmeier, M ........... 85 Sun, H.J ............... 240 Suttan, J ............... 284 Swinford, S ............. 214 Swoboda, M ............. 284 Tropea, C .............. 85 Vermeulen, J.P ...........178 Vollan, A .............. 10 Waitz, LA .............. 246 Wang, H.M............. 392 Webster, L .............. 359 Wendt, J.F.............. 178 Wong, D.T ............. 382 Wright, R.E., Jr .......... 156 Yamaguchi, Y............ 223 Yan, Y.Y ............82, 94 Yano, К ...............277 Yanta, WJ .............136 Yorozu, M ..............223 Zhang, В ...............255 Zuppardi, G ............. 49
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spellingShingle ICIASF '91 record Rockvolle, Maryland, USA, October 27 - 31, 1991
Aerodynamic measurements Congresses
Aeronautics Research Congresses
Wind tunnels Congresses
Simulation (DE-588)4055072-2 gnd
Messtechnik (DE-588)4114575-6 gnd
Luftfahrttechnik (DE-588)4168244-0 gnd
subject_GND (DE-588)4055072-2
(DE-588)4114575-6
(DE-588)4168244-0
(DE-588)1071861417
title ICIASF '91 record Rockvolle, Maryland, USA, October 27 - 31, 1991
title_auth ICIASF '91 record Rockvolle, Maryland, USA, October 27 - 31, 1991
title_exact_search ICIASF '91 record Rockvolle, Maryland, USA, October 27 - 31, 1991
title_full ICIASF '91 record Rockvolle, Maryland, USA, October 27 - 31, 1991
title_fullStr ICIASF '91 record Rockvolle, Maryland, USA, October 27 - 31, 1991
title_full_unstemmed ICIASF '91 record Rockvolle, Maryland, USA, October 27 - 31, 1991
title_short ICIASF '91 record
title_sort iciasf 91 record rockvolle maryland usa october 27 31 1991
title_sub Rockvolle, Maryland, USA, October 27 - 31, 1991
topic Aerodynamic measurements Congresses
Aeronautics Research Congresses
Wind tunnels Congresses
Simulation (DE-588)4055072-2 gnd
Messtechnik (DE-588)4114575-6 gnd
Luftfahrttechnik (DE-588)4168244-0 gnd
topic_facet Aerodynamic measurements Congresses
Aeronautics Research Congresses
Wind tunnels Congresses
Simulation
Messtechnik
Luftfahrttechnik
Konferenzschrift 1991 Rockville Md.
url http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=003755711&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
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