International Congress on Instrumentation in Aerospace Simulation Facilities,
Latest Publications

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A further step to the LDA-Sensor: Concept for the Miniature Signal Processing Unit

International Congress on Instrumentation in Aerospace Simulation Facilities, ◽

10.1109/iciasf.1993.687674 ◽

2005 ◽

Author(s):

S. Damp ◽

E. Sommer

Keyword(s):

Signal Processing ◽

Processing Unit ◽

Signal Processing Unit

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Additional Developments of the Optical Pressure Measurement System (OPMS) for Non-flat Models and Unsteady Flow Conditions

International Congress on Instrumentation in Aerospace Simulation Facilities, ◽

10.1109/iciasf.1993.687693 ◽

2005 ◽

Author(s):

R.H. Engler

Keyword(s):

Unsteady Flow ◽

Measurement System ◽

Pressure Measurement ◽

Flow Conditions ◽

Optical Pressure ◽

Pressure Measurement System

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Goertler Vortices in Hypersonic Flow Detected by IR Thermography

International Congress on Instrumentation in Aerospace Simulation Facilities, ◽

10.1109/iciasf.1993.687646 ◽

2005 ◽

Author(s):

L. de Luca ◽

G. Cardone ◽

G.M. Carlomagno

Keyword(s):

Hypersonic Flow ◽

Ir Thermography

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Three-Dimensional Particle Image Velocimetry by Optical Processing of Holographic Records

International Congress on Instrumentation in Aerospace Simulation Facilities, ◽

10.1109/iciasf.1993.687682 ◽

2005 ◽

Cited By ~ 1

Author(s):

C.S. Moraitis

Keyword(s):

Particle Image Velocimetry ◽

Particle Image ◽

Three Dimensional ◽

Optical Processing ◽

Image Velocimetry

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Application of Spectroscopic Diagnostic Techniques to Studies on HEG: Preparatory LIF Work and Emission Spectroscopy Results

International Congress on Instrumentation in Aerospace Simulation Facilities, ◽

10.1109/iciasf.1993.687652 ◽

2005 ◽

Cited By ~ 3

Author(s):

W.H. Beck ◽

M. Muller ◽

M. Wollenhaupt

Keyword(s):

Emission Spectroscopy ◽

Diagnostic Techniques

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Skin Friction end Heat Transfer Measurements in Mach 6 High Reynolds Number Flows

International Congress on Instrumentation in Aerospace Simulation Facilities, ◽

10.1109/iciasf.1993.687662 ◽

2005 ◽

Cited By ~ 1

Author(s):

M.J. Wagner

Keyword(s):

Heat Transfer ◽

Reynolds Number ◽

Skin Friction ◽

High Reynolds Number ◽

High Reynolds ◽

Reynolds Number Flows

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An Experimental Study of the Stabilization of the Lifted Jet Diffusion Flame Using Molecular Rayleigh Scattering Technique

International Congress on Instrumentation in Aerospace Simulation Facilities, ◽

10.1109/iciasf.1993.687654 ◽

2005 ◽

Author(s):

Y.C. Chao ◽

M.J. Lee ◽

M.S. Jeng

Keyword(s):

Experimental Study ◽

Diffusion Flame ◽

Rayleigh Scattering ◽

Scattering Technique

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Instrumentation Highlights at Etw

International Congress on Instrumentation in Aerospace Simulation Facilities, ◽

10.1109/iciasf.1993.687644 ◽

2005 ◽

Cited By ~ 2

Author(s):

P.H. Fuykschot

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Experimental Analysis of Turbulent Structures by Means of Rapid Two-Component Laser-Doppler Scanning

International Congress on Instrumentation in Aerospace Simulation Facilities, ◽

10.1109/iciasf.1993.687680 ◽

2005 ◽

Cited By ~ 1

Author(s):

B. Lehmam ◽

J. Mante

Keyword(s):

Experimental Analysis ◽

Laser Doppler ◽

Turbulent Structures ◽

Two Component

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Application of Lda and Dgv to Complex High Speed Flows

International Congress on Instrumentation in Aerospace Simulation Facilities, ◽

10.1109/iciasf.1993.687681 ◽

2005 ◽

Author(s):

A.L. Heyes ◽

J.T. Turner

Keyword(s):

High Speed ◽

High Speed Flows

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International Congress on Instrumentation in Aerospace Simulation Facilities,Latest Publications

TOTAL DOCUMENTS

H-INDEX

Published By IEEE

A further step to the LDA-Sensor: Concept for the Miniature Signal Processing Unit

Additional Developments of the Optical Pressure Measurement System (OPMS) for Non-flat Models and Unsteady Flow Conditions

Goertler Vortices in Hypersonic Flow Detected by IR Thermography

Three-Dimensional Particle Image Velocimetry by Optical Processing of Holographic Records

Application of Spectroscopic Diagnostic Techniques to Studies on HEG: Preparatory LIF Work and Emission Spectroscopy Results

Skin Friction end Heat Transfer Measurements in Mach 6 High Reynolds Number Flows

An Experimental Study of the Stabilization of the Lifted Jet Diffusion Flame Using Molecular Rayleigh Scattering Technique

Instrumentation Highlights at Etw

Experimental Analysis of Turbulent Structures by Means of Rapid Two-Component Laser-Doppler Scanning

Application of Lda and Dgv to Complex High Speed Flows

International Congress on Instrumentation in Aerospace Simulation Facilities,
Latest Publications