Estimation of Surface Pressures from Observed Shock-wave Envelopes Surrounding Conical Bodies at M PDF Download
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Author: M. J. Larcombe
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
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Book Description
Author: M. J. Larcombe
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
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Book Description
Author: M. J. Larcombe
Publisher:
ISBN:
Category :
Languages : en
Pages : 17
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 652
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 22
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 850
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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 772
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Author: Library of Congress
Publisher:
ISBN:
Category :
Languages : en
Pages : 658
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 584
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Author: Allen Edward Winkelmann
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 60
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Book Description
A technique is outlined by which density gradients visible in two- dimensional schlieren photographs can be analyzed to obtain the density gradient structure (i.e., the shape and location of density gradients such as shock waves and vortices) of three-dimensional flow fields. Practical application of the technique relies on obtaining a series of schlieren photographs of the flow field from different viewing orientations. The analysis is specialized to the case of a right-circular cone at angle of attack. Results are presented which show the shape and location of the bow shock of a 5 deg half-angle right- circular cone at a nominal Mach number of 5.0, a nominal free-stream Reynolds number per foot of 4,800,000 and angles of attack equal to 15 and 40 deg.
Author: Great Britain. Her Majesty's Stationery Office
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 940
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