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A Method of Calculating Turbulent-boundary-layer Growth at Hypersonic Mach Numbers

A Method of Calculating Turbulent-boundary-layer Growth at Hypersonic Mach Numbers PDF Author: James C. Sivells
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 50

Book Description
A method is developed for calculating the growth of a turbulent boundary layer at hypersonic Mach numbers. Excellent agreement with experimental results from axisymmetric nozzles has been obtained by the application of this method. The method utilizes a modification of Stewartson's transformation to simplify the integration of the momentum equation. Heat transfer is taken into account by evaluating the gas properties at Eckert's reference temperature and by using a modification of Crocco's quadratic for the temperature distribution in the boundary layer. A new empirical relation is used for the incompressible friction coefficient which agrees with experimental data over a Reynold's number range from 10(superscript 5) to 10(superscript 9).

A Method of Calculating Turbulent-boundary-layer Growth at Hypersonic Mach Numbers

A Method of Calculating Turbulent-boundary-layer Growth at Hypersonic Mach Numbers PDF Author: James C. Sivells
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 50

Book Description
A method is developed for calculating the growth of a turbulent boundary layer at hypersonic Mach numbers. Excellent agreement with experimental results from axisymmetric nozzles has been obtained by the application of this method. The method utilizes a modification of Stewartson's transformation to simplify the integration of the momentum equation. Heat transfer is taken into account by evaluating the gas properties at Eckert's reference temperature and by using a modification of Crocco's quadratic for the temperature distribution in the boundary layer. A new empirical relation is used for the incompressible friction coefficient which agrees with experimental data over a Reynold's number range from 10(superscript 5) to 10(superscript 9).

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 784

Book Description


Some Turbulent Boundary-layer Measurements Obtained from the Forebody of an Airplane at Mach Numbers Up to 1.72

Some Turbulent Boundary-layer Measurements Obtained from the Forebody of an Airplane at Mach Numbers Up to 1.72 PDF Author: Edwin J. Saltzman
Publisher:
ISBN:
Category : Skin friction (Aerodynamics)
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Category : Aerodynamic heating
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Comparison of Prediction Methods and Studies of Relaxation in Hypersonic Turbulent Nozzle-wall Boundary Layers

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Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 44

Book Description
Turbulent boundary layer measurements on axisymmetric hypersonic nozzle walls.

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ISBN:
Category : Aeronautics
Languages : en
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