NASA Technical Note PDF Download
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 346
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 346
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Book Description
Author: M.D. Kelleher
Publisher: Elsevier
ISBN: 044459860X
Category : Technology & Engineering
Languages : en
Pages : 1002
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Book Description
The papers contained in this volume reflect the ingenuity and originality of experimental work in the areas of fluid mechanics, heat transfer and thermodynamics. The contributors are drawn from 27 countries which indicates how well the worldwide scientific community is networked. The papers cover a broad spectrum from the experimental investigation of complex fundamental physical phenomena to the study of practical devices and applications. A uniform outline and method of presentation has been used for each paper.
Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1050
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Book Description
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
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Book Description
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 556
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Book Description
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1680
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Book Description
Author: Clifford M. Akin
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 20
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Book Description
Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1732
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Book Description
Author:
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ISBN:
Category : Science
Languages : en
Pages : 232
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Book Description
Author: David Alexander Stewart
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 28
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Book Description
Heat-transfer rates were measured on large-angle conical bodies with large half-angles between 50 degrees and 90 degrees, at angles of attack from 0 degrees. The results at 0 degree angle of attack were predicted with Lees' similarity theory, using calculated flow properties at the boundary-layer edge. The calculated flow properties were obtained from Newtonian theory for the 50 degree cone and from a one- or two-strip solution using the method of integral relations for other cones. At 0 degree angle of attack, an increase in cone angle resulted in a decrease in the heating rate over much of the body. However, high heating rates occurred at the shoulder of the both the half-angle = 80 degree and half-angle =90 degree shapes because of local pressure gradients. On the windward side of the cones, the heating rate increased with angle of attack.
