Application of Digital Holographic Interferometry to Pressure Measurements of Symmetric, Supercritical and Circulation-control Airfoils in Transonic Flow Fields PDF Download
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Category :
Languages : en
Pages : 28
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Author:
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ISBN:
Category :
Languages : en
Pages : 28
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Author:
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Category : Aeronautics
Languages : en
Pages : 920
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Category :
Languages : en
Pages : 16
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Author:
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Category :
Languages : en
Pages : 26
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Author:
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Category :
Languages : en
Pages : 100
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Author:
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Category : Imaging systems
Languages : en
Pages : 300
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Author: Thomas Kreis
Publisher: John Wiley & Sons
ISBN: 3527604928
Category : Science
Languages : en
Pages : 554
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Book Description
The book presents the principles and methods of holographic interferometry - a coherent-optical measurement technique for deformation and stress analysis, for the determination of refractive-index distributions, or applied to non-destructive testing. Emphasis of the book is on the quantitative computer-aided evaluation of the holographic interferograms. Based upon wave-optics the evaluation methods, their implementation in computer-algorithms, and their applications in engineering are described.
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Category : Aeronautics
Languages : en
Pages : 666
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![Fluid Measurement[s] and Instrumentation Forum--1991 PDF](https://books.google.com/books/content/images/frontcover/bXMeAQAAIAAJ?fife=w80-h100)
Author: Robert Gore
Publisher:
ISBN:
Category : Fluid dynamic measurements
Languages : en
Pages : 140
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Author: Daniel Joseph Collins
Publisher:
ISBN:
Category : Holography
Languages : en
Pages : 126
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Book Description
The successful application of holographic interferometry to the study of density fields around opaque bodies in wind tunnel experiments has been reported in the literature. The present report extends this technique to the study of the asymmetric flow fields encountered near the wing-fuselage junction of an aerodynamic model in the transonic flow regime. Finite fringe interferometry has been used to investigate the three dimensional density field about a partially transparent wing-body structure. The resulting asymmetric density field and shock wave structure are shown to be an accurate representation of the phenomena encountered in aerodynamic corner flow. (Author).
