Investigation on Thermal Boundary Layer Around Heated Spinning Cone by Using 3D-Holographic Interferometry

The convective flow around a heated rotating cone of finite length is investigated experimentally by means of 3D and realtime holographic interferometry at rotational speeds up to 4600 rpm and rotational angles from 0 to 90. This advanced optical technique allows visualization of the thermal boundar...

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description The convective flow around a heated rotating cone of finite length is investigated experimentally by means of 3D and realtime holographic interferometry at rotational speeds up to 4600 rpm and rotational angles from 0 to 90. This advanced optical technique allows visualization of the thermal boundary layer. It's unstable transition region and the turbulent zones, as well as providing a detailed visual analysis of the holographic fringe patterns. Information about the thickness of the thermal boundary layer, and a new method for detecting and determining the critical points and critcal Reynolds numbers of the transition region. The results are compared with previously obtained experimental data. (Author) This article is from 'International Symposium on Applications of Laser Techniques to Fluid Mechanics and Workshop on Computers in Flow Measurements (6th) Held in Lisbon, Portugal on July 20-23, 1992', AD-A258 510, p35.4.1-35.4.6.
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C ; NATIONAL CHENG KUNG UNIV TAINAN (TAIWAN) INST OF AERONAUTICS AND ASTRONAUTIC S</creatorcontrib><description>The convective flow around a heated rotating cone of finite length is investigated experimentally by means of 3D and realtime holographic interferometry at rotational speeds up to 4600 rpm and rotational angles from 0 to 90. This advanced optical technique allows visualization of the thermal boundary layer. It's unstable transition region and the turbulent zones, as well as providing a detailed visual analysis of the holographic fringe patterns. Information about the thickness of the thermal boundary layer, and a new method for detecting and determining the critical points and critcal Reynolds numbers of the transition region. The results are compared with previously obtained experimental data. 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The results are compared with previously obtained experimental data. 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C</creatorcontrib><creatorcontrib>NATIONAL CHENG KUNG UNIV TAINAN (TAIWAN) INST OF AERONAUTICS AND ASTRONAUTIC S</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Tieng, S. M</au><au>Wang, Y. C</au><aucorp>NATIONAL CHENG KUNG UNIV TAINAN (TAIWAN) INST OF AERONAUTICS AND ASTRONAUTIC S</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Investigation on Thermal Boundary Layer Around Heated Spinning Cone by Using 3D-Holographic Interferometry</btitle><date>1992-07-23</date><risdate>1992</risdate><abstract>The convective flow around a heated rotating cone of finite length is investigated experimentally by means of 3D and realtime holographic interferometry at rotational speeds up to 4600 rpm and rotational angles from 0 to 90. 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source DTIC Technical Reports
subjects BOUNDARY LAYER TRANSITION
COMPARISON
Component Reports
CONVECTION(HEAT TRANSFER)
EXPERIMENTAL DATA
FLOW FIELDS
FLOW VISUALIZATION
Foreign reports
Holographic interferometry
Holography
Optical Detection and Detectors
OPTICAL INTERFEROMETERS
REYNOLDS NUMBER
ROTATION
SPATIAL DISTRIBUTION
TAIWAN
THERMAL BOUNDARY LAYER
Thermodynamics
THREE DIMENSIONAL
TURBULENCE
title Investigation on Thermal Boundary Layer Around Heated Spinning Cone by Using 3D-Holographic Interferometry
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