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Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44

Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 PDF Author: Earl A. Price
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 46

Book Description

Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44

Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 PDF Author: Earl A. Price
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 46

Book Description

Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44

Heat-transfer Measurements on a Flat Plate and Attached Fins at Mach Numbers of 3.51 and 4.44 PDF Author: Earl A. Price
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36

Book Description

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

Book Description

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

Heat-transfer Measurements on a Flat Plate and Attached Protuberances in a Turbulent Boundary Layer at Mach Numbers of 2.65, 3.51, and 4.44 PDF Author: Robert L. Stallings
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 246

Book Description

Heat-transfer and Pressure Measurements on a Flat-plate Surface and Heat-transfer Measurement on Attaches 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 Measurement on Attaches 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 :
Languages : en
Pages : 423

Book Description

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 :
Languages : en
Pages : 0

Book Description

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution PDF Author: Raul J. Conti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36

Book Description

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution

Heat-transfer Measurements at a Mach Number of 2 in the Turbulent Boundary Layer on a Flat Plate Having a Stepwise Temperature Distribution PDF Author: Raul Jorge Conti
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32

Book Description

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 : 423

Book Description

Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration

Free-flight Measurements of Aerodynamic Heat Transfer to Mach Number 3.9 and of Drag to Mach Number 6.9 of a Fin-stabilized Cone-cylinder Configuration PDF Author: Charles B. Rumsey
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 26

Book Description
Aerodynamic-heat-transfer measurements have been made at a station on the 10 degree total angle conical nose of a rocket-propelled model at flight Mach numbers of 1.4 to 3.9. The corresponding values of local Reynolds number varied from 18,000,000 to 46,000,000 and the ratio of skin temperature to local static temperature varied from 1.2 to 2.4. The experimental data, reduced to Stanton number, were in fair agreement with values predicted by Van Driest's theory for heat transfer on a cone with turbulent flow from the nose tip.
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