Heat Transfer to 36.75 and 45 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.70 to 2.99 and From 2.50 to 4.05 PDF Download

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Heat Transfer to 36.75 and 45 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.70 to 2.99 and From 2.50 to 4.05

Heat Transfer to 36.75 and 45 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.70 to 2.99 and From 2.50 to 4.05 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

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Heat Transfer to 36.75 and 45 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.70 to 2.99 and From 2.50 to 4.05

Heat Transfer to 36.75 and 45 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.70 to 2.99 and From 2.50 to 4.05 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

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Book Description

Heat Transfer to 36.75° and 45° Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.70 to 2.99 and from 2.50 to 4.05

Heat Transfer to 36.75° and 45° Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.70 to 2.99 and from 2.50 to 4.05 PDF Author: Robert L. O'Neal
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 37

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Book Description

Heat Transfer to 0° and 75° Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07

Heat Transfer to 0° and 75° Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 PDF Author: Robert L. O'Neal
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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Book Description

Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07

Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 PDF Author: Robert L. O'Neal
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 44

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Book Description

Heat Transfer to 0 Degree and 75 Degrees Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07

Heat Transfer to 0 Degree and 75 Degrees Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 PDF Author: ROBERT L. O'NEAL
Publisher:
ISBN:
Category :
Languages : en
Pages : 1

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A flight investigation of a rocket-powered model was conducted to study the heat transfer to wing leading edges in the vicinity of their juncture with a cylindrical body. Heat-transfer data were obtained on leading edges of 3/4-inch diameter at sweep angles of 0 and 75 degrees, Mach numbers from 1.90 to 3.07, and Reynolds numbers based on leading-edge diameter from 8.05 to 11.80 times 10 to the 5th power. The measured heating rates of both the 0 and 75 degrees swept leading edges were of the magnitude predicted by turbulent theory rather than by laminar theory. It is believed that the high level of heating observed on the leading edges was due to the influence of conditions existing in the turbulent boundary layer of the body. Comparison of the average measured heating on the cylindrical portions of both the swept and unswept leading edges indicates that the heating of the unswept segment was generally about twice that of the swept segment. (Author).

Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07

Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07 PDF Author: Robert L. O'Neal
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 38

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Analysis and Design of Flight Vehicle Structures

Analysis and Design of Flight Vehicle Structures PDF Author: Elmer Franklin Bruhn
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 1008

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Free-flight Measurements of Pressure and Heat Transfer on a Blunt Leading-edge Caret Wing at Design and Off-design MACH Numbers (M Equal 0.9 to 3.36

Free-flight Measurements of Pressure and Heat Transfer on a Blunt Leading-edge Caret Wing at Design and Off-design MACH Numbers (M Equal 0.9 to 3.36 PDF Author: Aeronautical Research Council
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Free-flight Measurements of Pressure and Heat Transfer on a Blunt Leading-edge Caret Wing at Design and Off-design Mach Numbers (M Infinity

Free-flight Measurements of Pressure and Heat Transfer on a Blunt Leading-edge Caret Wing at Design and Off-design Mach Numbers (M Infinity PDF Author: G.H. Greenwood
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Heat Transfer Coefficients for External Surfaces of Aircraft and Missiles for Flight at Mach Numbers Up to 5.0

Heat Transfer Coefficients for External Surfaces of Aircraft and Missiles for Flight at Mach Numbers Up to 5.0 PDF Author: Donald Robert Haworth
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 106

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Book Description