Preliminary Results from a Free-flight Investigation of Boundary-layer Transition and Heat Transfer on a Highly Polished 8-inch-diameter Hemisphere-cylinder at Mach Numbers Up to 3 and Reynolds Numbers Based on a Length of 1 Foot Up to 17.7 X 106 PDF Download
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Author: James R. Hall
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 34
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Book Description
Author: James R. Hall
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 34
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Book Description
Author: James J. Buglia
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 45
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Author: Alvin Seiff
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 654
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Book Description
Heat-transfer data from four wind-tunnel experiments and two free-flight experiments with turbulent boundary layers have been examined to see whether or not they are well represented by the Reynolds analogy or a modification thereof. The heat-transfer results are put into the form of dimensionless Stanton numbers based on fluid properties at the outer edge of the boundary layer and are compared with skin-friction coefficients for the same Mach numbers and wall to free-stream temperature ratios as obtained from an interpolation of the existing skin-friction data. The effective Reynolds number is taken to be the length Reynolds number measured from the effective turbulent origin, a position which differs importantly from the leading edge of the test surface in some cases.
Author: William D. Deveikis
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 30
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Author: James Rudyard Hall
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 186
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Author: Albert L. Braslow
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 20
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Author: Charles B. Rumsey
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 38
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Author: Robert L. O'Neal
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 44
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Author: Paul F. Holloway
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 54
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