Wind-tunnel Study of Oscillating Flow-induced Surface Pressures on a Tension-cone Geometry Model PDF Download
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Author: Frank P. Baltakis
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ISBN:
Category : Fluid mechanics
Languages : en
Pages : 62
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Book Description
Oscillating flow about a spiked body in a supersonic stream has been investigated in a wind tunnel at Mach 5 at free-stream unit Reynolds numbers of 2,500,000 to 20,000,000 per foot using fast-response pressure transducers, accelerometers and schlieren movie cameras. A tension-cone-type model with replaceable nosetips of two different lengths and two different surface roughnesses was used.
Author: Frank P. Baltakis
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 62
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Book Description
Oscillating flow about a spiked body in a supersonic stream has been investigated in a wind tunnel at Mach 5 at free-stream unit Reynolds numbers of 2,500,000 to 20,000,000 per foot using fast-response pressure transducers, accelerometers and schlieren movie cameras. A tension-cone-type model with replaceable nosetips of two different lengths and two different surface roughnesses was used.
Author:
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Category : Aeronautics
Languages : en
Pages : 702
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Author:
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ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 864
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Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
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Category : Aeronautics
Languages : en
Pages : 594
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ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 882
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Author:
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Category : Government publications
Languages : en
Pages : 1076
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Author:
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 472
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Author:
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ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1000
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Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1484
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1482
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