Heat Transfer and Boundary-layer Transition on Two Blunt Bodies at Mach Number 3.12 PDF Download

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Heat Transfer and Boundary-layer Transition on Two Blunt Bodies at Mach Number 3.12

Heat Transfer and Boundary-layer Transition on Two Blunt Bodies at Mach Number 3.12 PDF Author: N. S. Diaconis
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 31

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Book Description
Local heat-transfer parameters were measured on a hemisphere-cone-cylinder and on a 120 degree-included-angle cone-cylinder at a free-stream Mach number of 3.12 and at free-stream unit Reynolds numbers as high as 1,292.000 per inch. Heat-transfer data are presented for the case of wall temperature approximat&ly equal to free-stream static temperature.

Heat Transfer and Boundary-layer Transition on Two Blunt Bodies at Mach Number 3.12

Heat Transfer and Boundary-layer Transition on Two Blunt Bodies at Mach Number 3.12 PDF Author: N. S. Diaconis
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 31

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Book Description
Local heat-transfer parameters were measured on a hemisphere-cone-cylinder and on a 120 degree-included-angle cone-cylinder at a free-stream Mach number of 3.12 and at free-stream unit Reynolds numbers as high as 1,292.000 per inch. Heat-transfer data are presented for the case of wall temperature approximat&ly equal to free-stream static temperature.

The Influence of Low Wall Temperature on Boundary-layer Transition and Local Heat Transfer on 2-inch-diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X 106

The Influence of Low Wall Temperature on Boundary-layer Transition and Local Heat Transfer on 2-inch-diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X 106 PDF Author: Morton Cooper
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 42

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Correlation of Boundary-layer Transition Results on Highly Cooled Blunt Bodies

Correlation of Boundary-layer Transition Results on Highly Cooled Blunt Bodies PDF Author: Richard J. Wisniewski
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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The Influence of Low Wall Temperature on Boundary-Layer Transition and Local Heat Transfer on 2-Inch-Diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X 10(exp 6)

The Influence of Low Wall Temperature on Boundary-Layer Transition and Local Heat Transfer on 2-Inch-Diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X 10(exp 6) PDF Author: Morton Cooper
Publisher:
ISBN:
Category :
Languages : en
Pages : 50

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Analysis of Heat Transfer and Boundary Layer Transition on a Blunt Body at Hypersonic Speeds

Analysis of Heat Transfer and Boundary Layer Transition on a Blunt Body at Hypersonic Speeds PDF Author: Randall C. Maydew
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 43

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Effects of Mass Addition on Blunt-body Boundary-layer Transition and Heat Transfer

Effects of Mass Addition on Blunt-body Boundary-layer Transition and Heat Transfer PDF Author: George E. Kaattari
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 76

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Boundary-layer Transition Under Hypersonic Conditions

Boundary-layer Transition Under Hypersonic Conditions PDF Author: J. Leith Potter
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 128

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Local Afterbody Heat Transfer to a Blunt Two-dimensional Configuration at Mach 8

Local Afterbody Heat Transfer to a Blunt Two-dimensional Configuration at Mach 8 PDF Author: Dennis M. Bushnell
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 58

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Heat Transfer to Blunt Axially Symmetric Bodies

Heat Transfer to Blunt Axially Symmetric Bodies PDF Author: John O. Reller
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44

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Turbulent-boundary-layer Heat-transfer and Transition Measurements with Surface Cooling at Mach 6

Turbulent-boundary-layer Heat-transfer and Transition Measurements with Surface Cooling at Mach 6 PDF Author: Aubrey M. Cary
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 58

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