Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44 PDF Download

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Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44

Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44 PDF Author: Paige B. Burbank
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 30

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Book Description

Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44

Heat-Transfer and Pressure Measurements on a Flat-Face Cylinder at a Mach Number Range of 2.49 to 4.44 PDF Author: Paige B. Burbank
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 30

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Book Description

Heat-transfer and Pressure Measurements on Flat-face Cylinder at Mach Number Range of 2.49 to 4.44 [with List of References]

Heat-transfer and Pressure Measurements on Flat-face Cylinder at Mach Number Range of 2.49 to 4.44 [with List of References] PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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Book Description

Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44

Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44 PDF Author: Stallings, Jr. (Robert L.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 21

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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

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Book Description

Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90°

Heat-transfer Measurements on a Low-fineness-ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0° to 90° PDF Author: Philip E. Everhart
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44

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Book Description

Heat Transfer Measurements on a Low-fineness- Ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0 Deg to 90 Deg

Heat Transfer Measurements on a Low-fineness- Ratio Cylinder at a Mach Number of 10.4 and Angles of Attack from 0 Deg to 90 Deg PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 50

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Book Description

Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 ̊half-cone Body (semidisk) at a Mach Number of 6.15

Pressure and Heat-transfer Measurements on the Flat Face of a Blunted 10 ̊half-cone Body (semidisk) at a Mach Number of 6.15 PDF Author: P. Calvin Stainback
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 32

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Book Description

Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44

Heat-transfer and Pressure Measurements on a Concove-nose Cylinder for a Mach Number Range of 2.49 to 4.44 PDF Author: Stallings, Jr. (Robert L.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 21

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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

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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.

Heat-transfer and Pressure Measurements on Flat-faced Cylinders at a Mach Number of 2

Heat-transfer and Pressure Measurements on Flat-faced Cylinders at a Mach Number of 2 PDF Author: William E. Stoney
Publisher:
ISBN:
Category : Cylinders
Languages : en
Pages : 38

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Book Description
Flat-faced cylinders of 12-inch dtameter and 4-inch diameter were tested at a Mach number of 2 and sea-level conditions in the preflight jet of the Langley Pilotless Aircraft Research Station at Wallops Island, Va. Both pressure distributions and heat-transfer rates were measured.