Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers
Title | Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers PDF eBook |
Author | Ivan E. Beckwith |
Publisher | |
Pages | 32 |
Release | 1961 |
Genre | Hypersonic planes |
ISBN |
Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers
Title | Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers PDF eBook |
Author | Ivan E. Beckwith |
Publisher | |
Pages | 25 |
Release | 1961 |
Genre | Hypersonic planes |
ISBN |
Local heat transfer, equilibrium temperatures, and pressure have been measured on a circular cylinder for yaw angles from 0° to 60° and Reynolds numbers from 1X106 to 4X106. Increasing the yaw angle from 0° to 40° generally caused large increases in local heat-transfer coefficients followed by a decrease as the yaw angle was increased to 60°. The level of heating rates and the type if chordwise distribution indicated that a flow mechanism different from the conventional transitional boundary layer may exist for the intermediate yaw angles.
Local Heat Transfer and Recovery Temperatures on Yawed Cylinder at Mach Number of 4.15 and High Reynolds Numbers [with List of References]
Title | Local Heat Transfer and Recovery Temperatures on Yawed Cylinder at Mach Number of 4.15 and High Reynolds Numbers [with List of References] PDF eBook |
Author | |
Publisher | |
Pages | 6 |
Release | 1959 |
Genre | |
ISBN |
Local Heat Transfer and Recovery Temperatures on Yawed Cylinder at Mach Numbers of 4.15 and High Reynolds Numbers [with List of References]
Title | Local Heat Transfer and Recovery Temperatures on Yawed Cylinder at Mach Numbers of 4.15 and High Reynolds Numbers [with List of References] PDF eBook |
Author | |
Publisher | |
Pages | 25 |
Release | 1962 |
Genre | |
ISBN |
Temperature Recovery Factors on a Slender 12° Cone-cylinder at Mach Numbers from 3.0 to 6.3 and Angles of Attack Up to 45°
Title | Temperature Recovery Factors on a Slender 12° Cone-cylinder at Mach Numbers from 3.0 to 6.3 and Angles of Attack Up to 45° PDF eBook |
Author | John O. Reller |
Publisher | |
Pages | 64 |
Release | 1955 |
Genre | Aerodynamics |
ISBN |
Abstract: Temperature recovery factors were determined for a slender, thin-walled cone-cylinder, having a 12° vertex angle and a 1.25-inch-diameter cylinder, at Mach numbers from 3.02 to 6.30. The angle-of-attack range was 0° to 45° at Mach numbers up to 3.50, and about 0° to 20° at Mach numbers from 4.23 to 6.30. A transverse cylinder of the same diameter was also tested at Mach number 3.02. Free-stream Reynolds numbers varied from 1.8 to 11.0 million per foot. Flow visualization studies of boundary-layer transition and flow separation were made and the results correlated with recovery-factor measurements.
Computational Fluid Mechanics and Heat Transfer, Third Edition
Title | Computational Fluid Mechanics and Heat Transfer, Third Edition PDF eBook |
Author | Richard H. Pletcher |
Publisher | CRC Press |
Pages | 777 |
Release | 2012-08-30 |
Genre | Science |
ISBN | 1591690374 |
Thoroughly updated to include the latest developments in the field, this classic text on finite-difference and finite-volume computational methods maintains the fundamental concepts covered in the first edition. As an introductory text for advanced undergraduates and first-year graduate students, Computational Fluid Mechanics and Heat Transfer, Third Edition provides the background necessary for solving complex problems in fluid mechanics and heat transfer. Divided into two parts, the book first lays the groundwork for the essential concepts preceding the fluids equations in the second part. It includes expanded coverage of turbulence and large-eddy simulation (LES) and additional material included on detached-eddy simulation (DES) and direct numerical simulation (DNS). Designed as a valuable resource for practitioners and students, new homework problems have been added to further enhance the student’s understanding of the fundamentals and applications.
The Influence of Low Wall Temperature on Boundary-layer Transition and Local Heat Transfer on 2-inch-diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X 106
Title | The Influence of Low Wall Temperature on Boundary-layer Transition and Local Heat Transfer on 2-inch-diameter Hemispheres at a Mach Number of 4.95 and a Reynolds Number Per Foot of 73.2 X 106 PDF eBook |
Author | Morton Cooper |
Publisher | |
Pages | 42 |
Release | 1960 |
Genre | Aerodynamics, Hypersonic |
ISBN |