Practical Aspects of Laser Holographic Interferometry in Wind Tunnels PDF Download
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Languages : en
Pages : 20
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Languages : en
Pages : 20
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Author: Tse-Fou Zien
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Category : Holographic interferometry
Languages : en
Pages : 120
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Holographic interferometry was successfully applied to a large-scale wind tunel (40-cm x 40-cm test section) experiment on a three-dimensional flow field. The laser interferometer was set up in a schlieren bench with a pulsed-ruby laser as the light source. Both the object beam and the reference beam were collimated. The conventional double-exposure, off-axis operation was used to produce interferograms...
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Category : Aeronautics
Languages : en
Pages : 488
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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Pages : 0
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Holographic interferometry was successfully applied to a large-scale wind tunnel (40-cm x 40-cm test section) experiment on a three-dimensional flow field. The laser interferometer was set up in a schlieren bench with a pulsed-ruby laser as the light source. Both the object beam and the reference beam were collimated. The conventional double-exposure, off-axis operation was used to produce interferograms. A 15-degree half-angle opaque cone at zero and 16.5 degrees yaw in a M = 2 free stream provided the flow field for the investigation. The aerodynamic conditions were such that flow field was largely inviscid.
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Languages : en
Pages : 102
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Holographic interferometry was successfully applied to a large-scale wind tunnel (40-cm x 40-cm test section) experiment on a three-dimensional flow field. The laser interferometer was set up in a schlieren bench with a pulsed-ruby laser as the light source. Both the object beam and the reference beam were collimated. The conventional double-exposure, off-axis operation was used to produce interferograms. A 15-degree half-angle opaque cone at zero and 16.5 degrees yaw in a M = 2 free stream provided the flow field for the investigation. The aerodynamic conditions were such that flow field was largely inviscid.
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Languages : en
Pages : 64
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Pages : 16
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Author: B. G. Ponseggi
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Category : Image processing
Languages : en
Pages : 230
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Category : Aeronautics
Languages : en
Pages : 668
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Category : Government publications
Languages : en
Pages : 1168
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