3 edition of Unsteady three-dimensional marginal separation, including breakdown found in the catalog.
Unsteady three-dimensional marginal separation, including breakdown
Peter W. Duck
by NASA, Institute for Computational Mechanics in Propulsion, NASA Lewis Research Center, Case Western Reserve University, For sale by the National Technical Information Service in [Washington, D.C.], [Cleveland, Ohio], [Springfield, Va
Written in English
|Other titles||Unsteady three dimensional marginal separation, including breakdown.|
|Statement||Peter W. Duck.|
|Series||NASA technical memorandum -- 102525.|
|Contributions||Lewis Research Center. Institute for Computational Mechanics in Propulsion.|
|The Physical Object|
|Pagination||29 p. :|
|Number of Pages||29|
Shock-induced three-dimensional separation of an axisymmetric hypersonic turbulent boundary layer. Review of skin friction measurements including recent high-Reynolds number results from NASA Langley NTF. A high-speed time resolved DPIV study of the unsteady characteristics of vortex breakdown. An innovative model based on the vortex theory is presented with the aim of simulating the two-dimensional airfoil dynamic behavior at pitching reduced frequencies related to vertical axis wind-turbine operative conditions. The model relies on the introduction of a second separated wake from the suction side to correctly account for the aerodynamic effects of stall conditions and is provided.
Prevailing utilization of airfoils in the design of micro air vehicles and wind turbines causes to gain attention in terms of determination of flow characterization on these flight vehicles operating at low Reynolds numbers. Thus, these vehicles require flow control techniques to reduce flow phenomena such as boundary layer separation or laminar separation bubble (LSB) affecting aerodynamic. Vortex breakdown, vortex control, and the effect of compressibility on these three- dimensional flows as well as the present and future capabilities of computational techniques are discussed. These fundamental lectures are supplemented by a description of the techniques currently employed by combat aircraft and missile design groups.
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The three-dimensional marginal separation of a boundary layer along a line of symmetry is considered. The key equation governing the displacement function is derived, and found to be a nonlinear integral equation in two space by: Unsteady three-dimensional marginal separation, including.
Zametaev, Vik V. Sychev, Three-dimensional separation in the neighborhood of roughness on the surface of an axisymmetric body, Fluid Dynamics, /BF, 30, 3. A situation involving a three-dimensional marginal separation is considered, where a (steady) boundary layer flow is on the verge of separating at a point (located along a line of symmetry/centerline).
At this point, a triple-deck is included, thereby permitting a small amount of interaction to occur. Including breakdown book is included within this interaction region through some external : Peter W.
Duck. Unsteady three-dimensional marginal separation, including breakdown. By Peter W. Duck. Abstract. A situation involving a three-dimensional marginal separation is considered, where a (steady) boundary layer flow is on the verge of separating at a point (located along a line of symmetry/centerline).
It is shown that the problem reduces to Author: Peter W. Duck. A situation involving a three-dimensional marginal separation is considered, where a (steady) boundary layer flow is on the verge of separating at a point (located along a line of symmetry. Unsteady Unsteady three-dimensional marginal separation marginal separation, including breakdown by linear and nonlinear analysis suggest that with confined initial conditions the strong instabilities in the present unsteady flow tend to force a breakdown within a finite time.
Unsteady three-dimensional marginal separation, including breakdown. Journal of Fluid. Braun, S., Kluwick, A. Unsteady three-dimensional marginal separation caused by surface-mounted obstacles and/or local suction, J. Fluid Mech. –. Braun S., Kluwick A.: Unsteady three-dimensional marginal separation caused by surface mounted obstacles and/or local suction.
Fluid Mech. – () zbMATH CrossRef MathSciNet Google Scholar. UNSTEADY THREE-DIMENSIONAL MARGINAL SEPARATION. INCLUDING BREAKDOWN Peter W. Duck Department of Mathematics University of Manchester Manchester, England and Institute for Computational Mechanics in Propulsion* Lewis Research Center Cleveland, Ohio Abstract We consider a situation involving a three-dimensional marginal.
Get this from a library. Unsteady three-dimensional marginal separation, including breakdown. [Peter W Duck; Lewis Research Center. Institute for Computational Mechanics in Propulsion.]. An important issue in the present context concerns the inclusion of three-dimensional effects.
Unsteady marginal separation of a three-dimensional boundary layer on a line of symmetry has been investigated by Duck , who also worked out the terminal similarity structure of a blow-up event, in analogy to . The complicated unsteady and three-dimensional vortex wake is responsible for many peculiar the emergence of a singularity signals the breakdown of the boundary-layer approximation.
The case in which the point of zero shear stress forms adjacent to the surface at a velocity minimum in the context of marginal separation was considered by.
J.S. Carlton FREng, in Marine Propellers and Propulsion (Fourth Edition), Leading Edge Vortex. The origin of the leading edge vortex does not always coincide with local tip vortex. It frequently originates at the inner radii of the propeller blade because at those locations the blade loading is generally higher and, more importantly, the geometric curvature of the blade leading.
"Unsteady three-dimensional marginal separation caused by surface mounted obstacles and/or local suction"; Journal of Fluid Mechanics, (), - More information S. Braun, A. Kluwick: "Analysis of a bifurcation problem in marginally separated laminar wall jets and boundary layers"; Acta Mechanica, (), ; - The IUTAM Symposium on Boundary-Layer Separation, suggested by the UK National Committee of Theoretical and Applied Mechanics and supported by the International Union of Theoretical and Applied Mechanics, was held at University College London on August 26.
Extension of the familiar concept of boundary-layer separation to flow along moving walls and unsteady flows is a subject that attracted some interest in the ’s and has been investigated further in the past few years. The well-known criterion of vanishing wall-shear does not apply in such flows, and therefore the definition of the phenomenon becomes more difficult than in the simpler.
Therefore, three-dimensional, compressible, unsteady, Reynolds-averaged-Navier-Stokes numerical investigations are performed to illustrate motion-induced unsteady effects on transverse jet interaction.
Two pitch motion types, including forced-oscillation and free-response-motion, were chosen to evaluate the potential effects. Separation and reattachment near the leading edge of a thin wing.- Simulation of three-dimensional boundary-layer separation.- Separating flow: small-scale, large-scale, and nonlinear unsteady effects.- Session Breakdown of steady and unsteady interacting boundary layers.- Asymptotic separation from slender cones at incidence.- Poster Session based on unsteady marginal separation which reproduces some of the observed features.
Alternative paths to stall or transition involving some unsteady separation are studied by Peridier, Smith & Walker ( a, b), Hoyle, Smith & Walker (), Smith & Bowles (), Smith (). Our concern likewise is with unsteady separation and.
Duck P and Dry S L On a class of unsteady, non-parallel, three-dimensional disturbances to boundary-layer flows J. Fluid Mech. Crossref Google Scholar Elbashbeshy E M A and Basid M A A Heat transfer over an unsteady stretching surface Heat Mass Transfer 41 Large Eddy Simulations are carried out to analyze flow past flat plate in different configurations and inclinations.
A thin flat plate is considered at three inclination angles (α = 30°, 60° and 90°) and three aspect ratios (AR =2 and 5). The Reynolds number based on the free stream velocity and chord length of the plate at different inclination angles varies betw to ,Separated flows and jets are closely linked in a variety of applications.
They are of great importance in various fields of fluid mechanics including vehicle efficiency, technical branches concerned with gas/liquid flows, atmospheric effects on various constructions, etc.
Knowledge of the physics.