An Extension of the Investigation of the Effects of Heat Transfer on Boundary-layer Transition on a Parabolic Body of Revolution (NACA RM-10) at a Mach Number of 1.61
Title | An Extension of the Investigation of the Effects of Heat Transfer on Boundary-layer Transition on a Parabolic Body of Revolution (NACA RM-10) at a Mach Number of 1.61 PDF eBook |
Author | K. R. Czarnecki |
Publisher | |
Pages | 21 |
Release | 1954 |
Genre | Body of revolution |
ISBN |
The results indicate that the trend found previously of an increase in boundary-layer transition Reynolds number with increase in model cooling continued to higher Reynolds numbers. The highest transition Reynolds number obtained with cooling was 28,500,000. At this Reynolds number, the classical Tollmien-Schlichting wave type of boundary-layer number, the instability was apparently overshadowed by surface roughness effects. The results indicated that, when transition was fixed by surface irregularities or airstream flow disturbances, cooling was not effective in obtaining laminar flow behind the irregularity or disturbances.
Journal of the Royal Aeronautical Society
Title | Journal of the Royal Aeronautical Society PDF eBook |
Author | |
Publisher | |
Pages | 976 |
Release | 1956 |
Genre | Aeronautics |
ISBN |
The Journal of the Royal Aeronautical Society
Title | The Journal of the Royal Aeronautical Society PDF eBook |
Author | Royal Aeronautical Society |
Publisher | |
Pages | 938 |
Release | 1954 |
Genre | Aeronautics |
ISBN |
Handbook of Supersonic Aerodynamics
Title | Handbook of Supersonic Aerodynamics PDF eBook |
Author | D. Adamson |
Publisher | |
Pages | 366 |
Release | 1961 |
Genre | Aerodynamics, Supersonic |
ISBN |
Applied Mechanics Reviews
Title | Applied Mechanics Reviews PDF eBook |
Author | |
Publisher | |
Pages | 608 |
Release | 1955 |
Genre | Mechanics, Applied |
ISBN |
Handbook of Supersonic Aerodynamics
Title | Handbook of Supersonic Aerodynamics PDF eBook |
Author | Johns Hopkins University. Applied Physics Laboratory |
Publisher | |
Pages | 372 |
Release | 1961 |
Genre | Aerodynamics, Supersonic |
ISBN |
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 |