Heat Transfer from Cylinders Having Closely Spaced Fins PDF Download
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Author: Arnold E. Biermann
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 622
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Book Description
The use of baffles for directing the air around the cylinders with closely spaced fins proved very effective in increasing the over-all heat-transfer coefficient provided that the spacing was not appreciably less than that for maximum heat transfer.
Author: Arnold E. Biermann
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 622
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Book Description
The use of baffles for directing the air around the cylinders with closely spaced fins proved very effective in increasing the over-all heat-transfer coefficient provided that the spacing was not appreciably less than that for maximum heat transfer.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 698
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Author: Armour Research Foundation (U.S.)
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 84
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This report is the summary of a literature survey and analytical study performed by the Armour Research Foundation for NEPA on the subject of the effect of turbulence promotion on forced convection heat transfer and fluid friction.
Author: Albert Sherman
Publisher:
ISBN:
Category : Aiprlanes
Languages : en
Pages : 534
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Book Description
As part of the wing-fuselage interferences investigation in progress in the N.A.C.A. variable-density wind tunnel, a method of eliminating the interference burble associated with critical midwing combinations was investigated. The interference burble of the critical midewing combination was shown to respond to modifications at the nose of the juncture and to be entirely suppressed with little or no adverse effect on the high-speed drag by special leading-edge fillets.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 42
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Author: Franklin Moore
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 756
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Book Description
First-order relations were obtained for attenuation of shock and flow deflection outward along the shock. These relations probably conform closely to physical fact, provided the entrance slope is small. These relations contain an error, but become exact as the radial coordinate approaches inifinity. The error is thus probably of the second order over the entire shock front.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
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Author:
Publisher:
ISBN:
Category : Roads
Languages : en
Pages : 784
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Author:
Publisher:
ISBN:
Category : Roads
Languages : en
Pages : 786
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Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878
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