NEYLAND, 1970 - Google Patents
Propagation of disturbances above the flow during the interaction of a hypersonic flow with a boundary layer(Turbulence diffusion above flow during boundary layer …NEYLAND, 1970
- Document ID
- 4698571114877778871
- Author
- NEYLAND V
- Publication year
External Links
- 230000003993 interaction 0 title description 4
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Willmarth et al. | Measurements of the correlation between the fluctuating velocities and the fluctuating wall pressure in a thick turbulent boundary layer layer(Correlation between fluctuating velocities and fluctuating wall pressure in thick turbulent boundary layer) | |
| NEYLAND | Propagation of disturbances above the flow during the interaction of a hypersonic flow with a boundary layer(Turbulence diffusion above flow during boundary layer and hypersonic flow interaction) | |
| GEBEL et al. | Study of a hydrodynamic boundary layer- Evolution of the flow past obstacles in the presence of injection of non-Newtonian fluid into the boundary layer(Flow past streamlined obstacles under nonNewtonian fluid injection into hydrodynamic laminar and turbulent boundary layer) | |
| STOLLERY | Hypersonic viscous flow over concave and convex surfaces(Hypersonic laminar boundary layer growth over concave and convex surfaces) | |
| KOZLOV | Effect of gas compressibility on the transition of a laminar boundary layer into a turbulent one(Effect of gas compressibility on transition of laminar boundary layer into turbulent boundary layer) | |
| MICHALKE | Mechanical or acoustically induced disturbance studies in the free-stream boundary layer resulting in laminar turbulent transition | |
| TANI | Flat and concave plate boundary layer transition for unstable laminar flow | |
| BOGDONOFF | The laminar hypersonic boundary layer- Some observations of the leading and trailing edge problem(Limits of hypersonic boundary layer theory, and leading and trailing edge phenomena in laminar hypersonic boundary layer) | |
| DEMETRIADES | Wedge tests in hypersonic flow relate wake thickness and transition distance to the surface laminar boundary layer | |
| Prudnikov et al. | Diffusion and vortex models of the turbulent jet(Turbulent jet diffusion and vortex models, noting velocity profile in mixing and turbulent boundary layers) | |
| JACKSON | Investigation of the relationship between static- hole error and velocity distribution in the boundary layer | |
| MIRELS | Boundary layer growth effects in shock tubes(Laminar and turbulent wall boundary layer and shock attenuation effects on flow uniformity in shock tubes) | |
| Crabtree | An experimental investigation of the velocity and temperature profiles in the boundary layer above an unstable evaporating film of liquid under the influence of a moving stream of hot gas(Velocity and temperature profiles in boundary layer above unstable evaporating film under influence of hot gas stream) | |
| FRUMAN | Analog calculation of the form of immersed profiles in the presence of a free surface in subcavitating and supercavitating flow(Analog calculation of form of immersed profiles in presence of free surface in subcavitating and supercavitating flow) | |
| HAYASI | Investigation of effects of surface curvature on laminar boundary layer flow | |
| FANG | Velocity defect law for the turbulent boundary layer with injection or suction at the wall(Velocity defect law for turbulent incompressible boundary layer with wall injection or suction) | |
| LEBOUCHE | Relation between the mass-transfer and velocity-gradient fluctuations at the wall in the case of large Schmidt numbers(Mass transfer and velocity gradient fluctuations at wall in two dimensional or rotational flow for large Schmidt numbers) | |
| KOZLOV | Asymptotic boundary layer in a compressible gas in the presence of normal and tangential velocity components at the surface of the body(Asymptotic laminar boundary layer in compressible gas in presence of normal and tangential velocity components at body surface) | |
| HRUBECKY et al. | The effect of injection upon the turbulent boundary layer on a cone in supersonic flow(Differential equation for boundary layer thickness and friction coefficient for turbulent boundary layer subject to injection developed on cone in supersonic flow) | |
| ROTTA | On the relation between the local skin friction coefficients of a turbulent boundary layer in compressible and incompressible flow(Relation between skin friction of turbulent boundary layer in compressible and incompressible flow) | |
| MARECHAL | Numerical method of solving the equations of the bidimensional, compressible, laminar boundary layer(Compressible laminar boundary layer equations solved, noting wall flow and suction problem application) | |
| TEWFIK | Measurements of velocity profiles for a turbulent boundary layer with air injection | |
| DUHAMEL | Power density spectrum of the fluctuations of the longitudinal velocity component in a pretransition pulsed boundary layer(Power density spectrum of longitudinal velocity fluctuations in pretransition pulsed boundary layer) | |
| WEINBAUM | Near wake uniqueness and a re-examination of the throat concept in laminar mixing theory(Near wake uniqueness and criticality condition in Crocco-Lees mixing theory, obtaining critical point from boundary layer equations of motion) | |
| TEWFIK | Porous surface roughness effects on turbulent boundary layer growth, skin friction, velocity and shear stress distribution |