This publication develops the first correlation equation between the theoretical turbulent skin friction with Preston-tube measurements on a subsonic cone. Lecturers, scientists, and practicing engineers in the field of fluid dynamics should be interested in this development. The goals of this NASA sponsored research are in two fold: (1) to develop a new procedure which could be used to develop a correlation equation for correlating Preston-tube pressure measurements within turbulent boundary layers with the corresponding theoretical values of skin friction coefficient, and (2) to apply the procedure to a ten-degree cone in order to obtain the said correlation equation. The boundary layer conservation of mass, momentum, and energy equations are numerically solved. The inviscid pressure distribution is also numerically determined in order to specify the boundary conditions along the outer edge of the boundary layer. Finally, the Preston- tube pressure measurements are correlated to the corresponding theoretical skin friction coefficient values by means of a least-squares technique.

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**Book Description **Book Condition: New. Publisher/Verlag: LAP Lambert Academic Publishing | CORRELATION OF THEORETICAL TURBULENT SKIN FRICTION WITH PRESTON-TUBE MEASUREMENTS ON A SUBSONIC CONE | This publication develops the first correlation equation between the theoretical turbulent skin friction with Preston-tube measurements on a subsonic cone. Lecturers, scientists, and practicing engineers in the field of fluid dynamics should be interested in this development. The goals of this NASA sponsored research are in two fold: (1) to develop a new procedure which could be used to develop a correlation equation for correlating Preston-tube pressure measurements within turbulent boundary layers with the corresponding theoretical values of skin friction coefficient, and (2) to apply the procedure to a ten-degree cone in order to obtain the said correlation equation. The boundary layer conservation of mass, momentum, and energy equations are numerically solved. The inviscid pressure distribution is also numerically determined in order to specify the boundary conditions along the outer edge of the boundary layer. Finally, the Preston- tube pressure measurements are correlated to the corresponding theoretical skin friction coefficient values by means of a least-squares technique. | Format: Paperback | Language/Sprache: english | 128 pp. Bookseller Inventory # K9783838339054

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**Book Description **LAP Lambert Acad. Publ. Apr 2010, 2010. Taschenbuch. Book Condition: Neu. Neuware - This publication develops the first correlation equation between the theoretical turbulent skin friction with Preston-tube measurements on a subsonic cone. Lecturers, scientists, and practicing engineers in the field of fluid dynamics should be interested in this development. The goals of this NASA sponsored research are in two fold: (1) to develop a new procedure which could be used to develop a correlation equation for correlating Preston-tube pressure measurements within turbulent boundary layers with the corresponding theoretical values of skin friction coefficient, and (2) to apply the procedure to a ten-degree cone in order to obtain the said correlation equation. The boundary layer conservation of mass, momentum, and energy equations are numerically solved. The inviscid pressure distribution is also numerically determined in order to specify the boundary conditions along the outer edge of the boundary layer. Finally, the Preston- tube pressure measurements are correlated to the corresponding theoretical skin friction coefficient values by means of a least-squares technique. 128 pp. Englisch. Bookseller Inventory # 9783838339054

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**Book Description **LAP Lambert Acad. Publ. Apr 2010, 2010. Taschenbuch. Book Condition: Neu. Neuware - This publication develops the first correlation equation between the theoretical turbulent skin friction with Preston-tube measurements on a subsonic cone. Lecturers, scientists, and practicing engineers in the field of fluid dynamics should be interested in this development. The goals of this NASA sponsored research are in two fold: (1) to develop a new procedure which could be used to develop a correlation equation for correlating Preston-tube pressure measurements within turbulent boundary layers with the corresponding theoretical values of skin friction coefficient, and (2) to apply the procedure to a ten-degree cone in order to obtain the said correlation equation. The boundary layer conservation of mass, momentum, and energy equations are numerically solved. The inviscid pressure distribution is also numerically determined in order to specify the boundary conditions along the outer edge of the boundary layer. Finally, the Preston- tube pressure measurements are correlated to the corresponding theoretical skin friction coefficient values by means of a least-squares technique. 128 pp. Englisch. Bookseller Inventory # 9783838339054

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**Book Description **LAP Lambert Academic Publishing. Paperback. Book Condition: New. 128 pages. Dimensions: 8.7in. x 5.9in. x 0.3in.This publication develops the first correlation equation between the theoretical turbulent skin friction with Preston-tube measurements on a subsonic cone. Lecturers, scientists, and practicing engineers in the field of fluid dynamics should be interested in this development. The goals of this NASA sponsored research are in two fold: (1) to develop a new procedure which could be used to develop a correlation equation for correlating Preston-tube pressure measurements within turbulent boundary layers with the corresponding theoretical values of skin friction coefficient, and (2) to apply the procedure to a ten-degree cone in order to obtain the said correlation equation. The boundary layer conservation of mass, momentum, and energy equations are numerically solved. The inviscid pressure distribution is also numerically determined in order to specify the boundary conditions along the outer edge of the boundary layer. Finally, the Preston- tube pressure measurements are correlated to the corresponding theoretical skin friction coefficient values by means of a least-squares technique. This item ships from multiple locations. Your book may arrive from Roseburg,OR, La Vergne,TN. Paperback. Bookseller Inventory # 9783838339054

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**Book Description **LAP Lambert Acad. Publ. Apr 2010, 2010. Taschenbuch. Book Condition: Neu. This item is printed on demand - Print on Demand Neuware - This publication develops the first correlation equation between the theoretical turbulent skin friction with Preston-tube measurements on a subsonic cone. Lecturers, scientists, and practicing engineers in the field of fluid dynamics should be interested in this development. The goals of this NASA sponsored research are in two fold: (1) to develop a new procedure which could be used to develop a correlation equation for correlating Preston-tube pressure measurements within turbulent boundary layers with the corresponding theoretical values of skin friction coefficient, and (2) to apply the procedure to a ten-degree cone in order to obtain the said correlation equation. The boundary layer conservation of mass, momentum, and energy equations are numerically solved. The inviscid pressure distribution is also numerically determined in order to specify the boundary conditions along the outer edge of the boundary layer. Finally, the Preston- tube pressure measurements are correlated to the corresponding theoretical skin friction coefficient values by means of a least-squares technique. 128 pp. Englisch. Bookseller Inventory # 9783838339054

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**Book Description **LAP Lambert Academic Publishing, Germany, 2010. Paperback. Book Condition: New. Language: English . Brand New Book. This publication develops the first correlation equation between the theoretical turbulent skin friction with Preston-tube measurements on a subsonic cone. Lecturers, scientists, and practicing engineers in the field of fluid dynamics should be interested in this development. The goals of this NASA sponsored research are in two fold: (1) to develop a new procedure which could be used to develop a correlation equation for correlating Preston-tube pressure measurements within turbulent boundary layers with the corresponding theoretical values of skin friction coefficient, and (2) to apply the procedure to a ten-degree cone in order to obtain the said correlation equation. The boundary layer conservation of mass, momentum, and energy equations are numerically solved. The inviscid pressure distribution is also numerically determined in order to specify the boundary conditions along the outer edge of the boundary layer. Finally, the Preston- tube pressure measurements are correlated to the corresponding theoretical skin friction coefficient values by means of a least-squares technique. Bookseller Inventory # KNV9783838339054

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