ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025)

2003 ◽

Author(s):

Y. Yamaguchi ◽

M. Kashitani ◽

K. Kaibara ◽

T. Saito

Keyword(s):

Wind Tunnel ◽

Cryogenic Wind Tunnel

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Pressure-sensitive-paint measurements in a large-scale commercial-engine test stand

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) ◽

10.1109/iciasf.1999.827161 ◽

2003 ◽

Cited By ~ 2

Author(s):

J.D. Jordan ◽

A.N. Watkins ◽

J.C.P.N. Davis ◽

W.L. Weaver ◽

G.A. Dale ◽

...

Keyword(s):

Large Scale ◽

Test Stand ◽

Engine Test ◽

Pressure Sensitive Paint ◽

Pressure Sensitive

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Measurement technology of the impact of alumina liquid particles on a hot surface

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) ◽

10.1109/iciasf.1999.827151 ◽

2003 ◽

Author(s):

C. Escure ◽

M. Vardelle ◽

A. Grimaud ◽

P. Fauchais

Keyword(s):

Measurement Technology ◽

Hot Surface ◽

The Impact

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Development and applications of a rapid flight test prototyping system for unmanned air vehicles

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) ◽

10.1109/iciasf.1999.827166 ◽

2003 ◽

Cited By ~ 2

Author(s):

E. Hallberg ◽

J. Komlosy ◽

T. Rivers ◽

M. Watson ◽

D. Meeks ◽

...

Keyword(s):

Flight Test ◽

Unmanned Air Vehicles ◽

Air Vehicles

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Half-model-balance for the Cologne-cryogenic-wind-tunnel development and test results

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) ◽

10.1109/iciasf.1999.827172 ◽

2003 ◽

Author(s):

K. Hufnagel ◽

R. Rebstock ◽

Junnai Zhai

Keyword(s):

Wind Tunnel ◽

Test Results ◽

Cryogenic Wind Tunnel

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An integrated approach to the application of high bandwidth optical pyrometry to turbine blade surface temperature mapping

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) ◽

10.1109/iciasf.1999.827143 ◽

2003 ◽

Cited By ~ 1

Author(s):

J. Douglas ◽

C.A. Smith ◽

S.J.R. Taylor

Keyword(s):

Surface Temperature ◽

Turbine Blade ◽

Integrated Approach ◽

Blade Surface ◽

Optical Pyrometry ◽

Temperature Mapping ◽

High Bandwidth

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Laser anemometer measurements in a centrifugal compressor

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) ◽

10.1109/iciasf.1999.827147 ◽

2003 ◽

Author(s):

N. Saddour ◽

A. Carrere

Keyword(s):

Centrifugal Compressor ◽

Laser Anemometer

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Application of the direct PSP-lifetime method on pyren-based paint as a completion of the existing DLR PSP system

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) ◽

10.1109/iciasf.1999.827163 ◽

2003 ◽

Author(s):

O. Trinks ◽

R.H. Engler ◽

C. Klein ◽

S. Fonov

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Pressure and temperature measurements with a dual-luminophor coating

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) ◽

10.1109/iciasf.1999.827158 ◽

2003 ◽

Author(s):

B.F. Carroll ◽

J.P. Hubner ◽

K. Schanze ◽

J. Bedlek ◽

M. Morris

Keyword(s):

Temperature Measurements

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Multiple point dynamic gas density measurements using molecular Rayleigh scattering

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025) ◽

10.1109/iciasf.1999.827183 ◽

2003 ◽

Author(s):

R. Seasholtz ◽

J. Panda

Keyword(s):

Rayleigh Scattering ◽

Multiple Point ◽

Gas Density ◽

Density Measurements

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ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025)
Latest Publications

TOTAL DOCUMENTS

H-INDEX

Published By IEEE

Feasibility of airfoil tests with a small high subsonic cryogenic wind tunnel

Pressure-sensitive-paint measurements in a large-scale commercial-engine test stand

Measurement technology of the impact of alumina liquid particles on a hot surface

Development and applications of a rapid flight test prototyping system for unmanned air vehicles

Half-model-balance for the Cologne-cryogenic-wind-tunnel development and test results

An integrated approach to the application of high bandwidth optical pyrometry to turbine blade surface temperature mapping

Laser anemometer measurements in a centrifugal compressor

Application of the direct PSP-lifetime method on pyren-based paint as a completion of the existing DLR PSP system

Pressure and temperature measurements with a dual-luminophor coating

Multiple point dynamic gas density measurements using molecular Rayleigh scattering

Export Citation Format

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025)Latest Publications

TOTAL DOCUMENTS

H-INDEX

Published By IEEE

Feasibility of airfoil tests with a small high subsonic cryogenic wind tunnel

Pressure-sensitive-paint measurements in a large-scale commercial-engine test stand

Measurement technology of the impact of alumina liquid particles on a hot surface

Development and applications of a rapid flight test prototyping system for unmanned air vehicles

Half-model-balance for the Cologne-cryogenic-wind-tunnel development and test results

An integrated approach to the application of high bandwidth optical pyrometry to turbine blade surface temperature mapping

Laser anemometer measurements in a centrifugal compressor

Application of the direct PSP-lifetime method on pyren-based paint as a completion of the existing DLR PSP system

Pressure and temperature measurements with a dual-luminophor coating

Multiple point dynamic gas density measurements using molecular Rayleigh scattering

ICIASF 99. 18th International Congress on Instrumentation in Aerospace Simulation Facilities. Record (Cat. No.99CH37025)
Latest Publications