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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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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Turbulent Boundary Layer Heat Transfer and Transition Measurements with Extreme Surface Cooling in Hypersonic Flow

Turbulent Boundary Layer Heat Transfer and Transition Measurements with Extreme Surface Cooling in Hypersonic Flow PDF Author: Aubrey Cary
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 154

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A Review of High-speed, Convective, Heat-transfer Computation Methods

A Review of High-speed, Convective, Heat-transfer Computation Methods PDF Author: Michael E. Tauber
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44

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Laminar, Transitional, and Turbulent Heat Transfer to a Cone-cylinder-flare Body at Mach 8.0

Laminar, Transitional, and Turbulent Heat Transfer to a Cone-cylinder-flare Body at Mach 8.0 PDF Author: Victor Zakkay
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 86

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A modified equation for the heat transfer coefficient in the transitional and fully turbulent region based on the F.P.R.E. method is then presented. This method gives good agreement with the experimental results presented here.

Measurements of a Mach 4.9 Zero-pressure-gradient Turbulent Boundary Layer with Heat Yransfer

Measurements of a Mach 4.9 Zero-pressure-gradient Turbulent Boundary Layer with Heat Yransfer PDF Author: Robert L. P. Voisinet
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 128

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The results of a detailed experimental investigation of the compressible turbulent boundary layer in a zero-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall for a nominal Mach number of 4.9, at momentum thickness Reynolds numbers from 7,000. to 58,000. and at wall-to-adiabatic-wall temperature ratios of 1.0, 0.8 and 0.25. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. Furthermore, the wall shear and surface heat transfer were measured directly with a skin-friction balance and a heat-transfer gage, respectively. (Author Modified Abstract).

Recovery Temperature Transition and Heat-transfer Measurements at Mach 5

Recovery Temperature Transition and Heat-transfer Measurements at Mach 5 PDF Author: Paul F. Brinich
Publisher:
ISBN:
Category :
Languages : en
Pages : 56

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Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44

Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurements on Attached Protuberances in a Supersonic Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 PDF Author: Paige B. Burbank
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 430

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 596

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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

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 Author: James R. Hall
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 34

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Laminar, Transition, and Turbulent Boundary-layer Heat-transfer Measurements with Wall Cooling in Turbulent Airflow Through a Tube

Laminar, Transition, and Turbulent Boundary-layer Heat-transfer Measurements with Wall Cooling in Turbulent Airflow Through a Tube PDF Author: L. H. Back
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 11

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