Organized Structures in a Supersonic Turbulent Boundary Layer
Title | Organized Structures in a Supersonic Turbulent Boundary Layer PDF eBook |
Author | Eric Francis Spina |
Publisher | |
Pages | 466 |
Release | 1988 |
Genre | Aerodynamics, Supersonic |
ISBN |
Organized Structures in a Supersonic Turbulent Boundary Layer
Title | Organized Structures in a Supersonic Turbulent Boundary Layer PDF eBook |
Author | Eric Francis Spina |
Publisher | |
Pages | 466 |
Release | 1988 |
Genre | Aerodynamics, Supersonic |
ISBN |
Fundamental Aspects of the Structure of Supersonic Turbulent Boundary Layers
Title | Fundamental Aspects of the Structure of Supersonic Turbulent Boundary Layers PDF eBook |
Author | Alexander J. Smits |
Publisher | |
Pages | 76 |
Release | 1988 |
Genre | Boundary layer |
ISBN |
Investigation of Supersonic Boundary Layer Transition and Turbulent Structure
Title | Investigation of Supersonic Boundary Layer Transition and Turbulent Structure PDF eBook |
Author | Alexander J. Smits |
Publisher | |
Pages | 40 |
Release | 1990 |
Genre | Rayleigh scattering |
ISBN |
Structure of the supersonic turbulent boundary layer and its influence on unsteady separation
Title | Structure of the supersonic turbulent boundary layer and its influence on unsteady separation PDF eBook |
Author | Ömer Haldun Ünalmiş |
Publisher | |
Pages | 510 |
Release | 1995 |
Genre | Turbulent boundary layer |
ISBN |
Fundamental Aspects of the Structure of Supersonic Turbulent Boundary
Title | Fundamental Aspects of the Structure of Supersonic Turbulent Boundary PDF eBook |
Author | Jonathan H. Watmuff |
Publisher | |
Pages | 41 |
Release | 1987 |
Genre | |
ISBN |
Measurements of structure angle in a supersonic turbulent boundary layer with zero and adverse pressure gradients are presented. Conditionally sampled measurements of u, v, and uv are presented along with quadrant analysis of the turbulent fluctuations. The latter suggests ambiguities associated with the interpretation of VITA measurements. Preliminary results of experiments on artificially generated hairpin vortices are also discussed. Measurements indicate a high degree of similarity between the signatures of these hairpin structures and ensemble averaged events in the turbulent boundary layer. Keywords: Turbulence, Boundary layer, Supersonic Flow.
On the Coupling Between a Supersonic Turbulent Boundary Layer and a Flexible Structure
Title | On the Coupling Between a Supersonic Turbulent Boundary Layer and a Flexible Structure PDF eBook |
Author | National Aeronautics and Space Administration (NASA) |
Publisher | Createspace Independent Publishing Platform |
Pages | 44 |
Release | 2018-07-09 |
Genre | |
ISBN | 9781722453923 |
A mathematical model and a computer code have been developed to fully couple the vibration of an aircraft fuselage panel to the surrounding flow field, turbulent boundary layer and acoustic fluid. The turbulent boundary layer model is derived using a triple decomposition of the flow variables and applying a conditional averaging to the resulting equations. Linearized panel and acoustic equations are used. Results from this model are in good agreement with existing experimental and numerical data. It is shown that in the supersonic regime, full coupling of the flexible panel leads to lower response and radiation from the panel. This is believed to be due to an increase in acoustic damping on the panel in this regime. Increasing the Mach number increases the acoustic damping, which is in agreement with earlier work. Frendi, Abdelkader Unspecified Center NAS1-19700; RTOP 537-06-37-20...