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An Influence of the Thickness of a Laminar Sublayer and Mixing Length Model on the Skin Friction and Heat Transfer in the Boundary Layer Flow
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J.W. Polkowski,
Published/Copyright:
June 1, 1995
Published Online: 1995-06
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Supersonic Axial Flow Oscillating Cascade Shock Motion and Unsteady Aerodynamic Moment
- An Influence of the Thickness of a Laminar Sublayer and Mixing Length Model on the Skin Friction and Heat Transfer in the Boundary Layer Flow
- The Generalized Untwist Problem of Rotating Blades: A Coupled Aeroelastic Formulation
- Effervescent Atomization and Internal Mixing Air Assist Atomization
- Low Speed Cascade Studies of Highly Cambered Single and Tandem Compressor Blading
- Fuel Injection Technique to Control the Flame Limits of a Twin-Plate Flameholder
- Linear Theory Modeling of Wakes in Radial Diffusers
Articles in the same Issue
- CONTENTS
- Supersonic Axial Flow Oscillating Cascade Shock Motion and Unsteady Aerodynamic Moment
- An Influence of the Thickness of a Laminar Sublayer and Mixing Length Model on the Skin Friction and Heat Transfer in the Boundary Layer Flow
- The Generalized Untwist Problem of Rotating Blades: A Coupled Aeroelastic Formulation
- Effervescent Atomization and Internal Mixing Air Assist Atomization
- Low Speed Cascade Studies of Highly Cambered Single and Tandem Compressor Blading
- Fuel Injection Technique to Control the Flame Limits of a Twin-Plate Flameholder
- Linear Theory Modeling of Wakes in Radial Diffusers
