3 edition of **Turbulence modeling of free shear layers for high-performance aircraft** found in the catalog.

Turbulence modeling of free shear layers for high-performance aircraft

- 325 Want to read
- 20 Currently reading

Published
**1993**
by MCAT Institute, National Aeronautics and Space Administration, National Technical Information Service, distributor in San Jose, CA, [Washington, DC, Springfield, Va
.

Written in English

- Turbulence -- Computer simulation.,
- Shear flow -- Computer simulation.

**Edition Notes**

Statement | Douglas L. Sondak. |

Series | NASA contractor report -- NASA CR-193659., MCAT Institute progress report -- 93-15. |

Contributions | United States. National Aeronautics and Space Administration. |

The Physical Object | |
---|---|

Format | Microform |

Pagination | 1 v. |

ID Numbers | |

Open Library | OL17679572M |

In physics and fluid mechanics, a boundary layer is the layer of fluid in the immediate vicinity of a bounding surface where the effects of viscosity are significant.. In the Earth's atmosphere, the atmospheric boundary layer is the air layer near the ground affected by diurnal heat, moisture or momentum transfer to or from the surface. On an aircraft wing the boundary layer is the part of the. This section includes the most commonlyused notation in this book. In ordertoavoiddeparting too muchfromconventionsnormally used in liter-ature on turbulence modeling andgeneral fluid mechanics, a few symbols denote more than one quantity. English Symbols Symbol Definition a Speedofsound aijkl Rapidpressure-strain tensor.

In addition to the need to develop innovative methods to control noise production by high speed shear layers, using a parabolized Navier-Stokes solver with a k — ε d two equation turbulence model with compressible turbulence dissipation. The predicted mean flow structure is used to apply the linearized compressible Rayleigh equation to. After carefull analysis in a turbulent zero-pressure gradient flow, various simple algebraic turbulence models were applied to the almost separated flow on the upperside of an airfoil at incidence. The Johnson-King and Horton non-equilibrium (or rate equation) models give clearly improved results.

Chapter 4 includes an expanded discussion of recent one-equation models, and presents a new version of the k-omega model that yields close agreement with measurements for both boundary layers with pressure gradient (for which the k-epsilon model is very inaccurate) and for classical free shear flows (for which the k-epsilon model is marginally Format: Paperback. Fares and W. Schröder, “ A general one-equation turbulence model for free shear and wall-bounded flows,” Flow, Turbul. Combust. Combust. 73, – ().

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A variety of free shear layers, including mixing layers over cavities, impinging jets, blown flaps, and exhaust plumes, may be encountered in such flowfields. Since these free shear layers are usually turbulent, ap- propriate turbulence models must be utilized in computations in order to accurately simulate these flow : Douglas L.

Sondak. Turbulence Modeling of Free Shear Layers For High Performance Aircraft Douglas Sondak In many flowfield computations, accuracy of the turbulence model employed is frequently a limiting factor in the overall accuracy of the computation.

This is particularly true for complex flowfields such as those around full aircraft configurations. Free shear. Get this from a library. Turbulence modeling of free shear layers for high performance aircraft. [Douglas L Sondak; United States. National Aeronautics and Space Administration.].

Turbulence modeling of free shear layers for high performance aircraft. accuracy of the turbulence model employed is frequently a limiting factor in the overall accuracy of the computation. This is particularly true for complex flowfields such as those around full aircraft configurations.

Free shear layers such as wakes, impinging jets (in Author: Douglas Sondak. Turbulence modeling of free shear layers for high-performance aircraft. By Douglas L. Sondak. Abstract. The High Performance Aircraft (HPA) Grand Challenge of Turbulence modeling of free shear layers for high-performance aircraft book High Performance Computing and Communications (HPCC) program involves the computation of the flow over a high performance aircraft.

A variety of free shear layers, including mixing Author: Douglas L. Sondak. Turbulence modeling is the construction and use of a mathematical model to predict the effects of ent flows are commonplace in most real life scenarios, including the flow of blood through the cardiovascular system, the airflow over an aircraft wing, the re-entry of space vehicles, besides others.

In spite of decades of research, there is no analytical theory to predict the. The modeling of turbulent free shear flows is crucial to the simulation of many aerospace applications, yet often receives less attention than the modeling of wall boundary layers. Thus, while turbulence model development in general has proceeded very slowly in the past twenty years, progress for free shear flows has been even more so.

NASA Technical Reports Server (NTRS) Turbulence modeling of free shear layers for high performance aircraft Item Preview. Turbulence models are developed by supplementing the renormalization group (RNG) approach of Yakhot and Orszag [J.

Sci. Comput. 1, 3 ()] with scale expansions for the Reynolds stress and production of dissipation terms. The additional expansion parameter (η≡SK̄/ ̄) is the ratio of the turbulent to mean strain time scale. While low‐order expansions appear to provide an adequate.

Turbulence is an irregular motion of the air resulting from eddies and vertical currents. It may be as insignificant as a few annoying bumps or severe enough to momentarily throw an airplane out of control or to cause structural damage.

Turbulence is associated with fronts, wind shear, thunderstorms, etc. THE PLANE FREE SHEAR LAYER 83 0 U c θ 0 /ν β x 1 / θ 0 (a) 0 1 0 β d θ /dx 1 (b) FIGURE (a) Location in which the velocity ﬂuctuations in a plane shear layer become self-sim-ilar, as a function of the initial boundary-layer Reynolds number.

Data from various experimenters. William K. Blake, in Mechanics of Flow-Induced Sound and Vibration, Volume 2 (Second Edition), Fundamental Half-Plane Problem. The high-frequency sound emitted from either the interaction of a sharp leading edge with upstream turbulence or the interaction of a trailing edge with the surface boundary layer turbulence is fundamentally a scattering phenomenon in which a high-wave.

(5). So, the general steps are: (a). the nature of boundary layer equation, (b). the process of Reynolds averaging, (c). the open-end Reynolds equation and Reynolds stresses, (d).

turbulence modeling for Reynolds stresses terms and the closure of the equations, (e). solution of governing equations along with the turbulence model and equations. (6). Lectures in Turbulence for the 21st Century William K. George Department of Aeronautics Imperial College of London London, UK and Professor of Turbulence Emeritus.

experienced by k-ε-type models are due to the modeling of the ε equation which is neither accurate or easy to solve (ε has a local extrema close to the wall) Mathematically this is equivalent to a change of variables ω∼ε/k The v2-f model is based on the argument that k/ε is the correct turbulent time.

The model parameters in turbulence models are often determined enforcing consistency in the prediction of fundamental ﬂows (e.g., homogeneous isotropic turbulence, logarithmic layer).

• Many turbulence models are based upon the Boussinesq hypothesis. – It was experimentally observed that turbulence decays unless there is shear in isothermal incompressible flows. – Turbulence was found to increase as the mean rate of deformation increases.

– Boussinesq proposed in that the Reynolds stresses could be. Dziomba, B. and Fiedler, H. Effect of initial conditions on two-dimensional free shear l of Fluid Mechanics, Vol. Issue., p. Keywords: Computational Fluid Dynamics (CFD), Airfoil, Aerodynamic Coefficients, Lift, Drag, Turbulence Models, Stalling, Boundary layer, Turbulence model, Angle of attack.: INTRODUCTION: The rapid evolution of computational fluid dynamics (CFD) has been driven by the need for faster and more accurate methods for the calculations of flow fields around configurations of technical interest.

A shear-free turbulent boundary layer - Volume 28 Issue 4 - T. Uzkan, W. Reynolds. Turbulence modeling of free shear layers for high-performance aircraft Douglas L.

Sondak Multiple-scale turbulence modeling of boundary layer flows for scramje G. Fabris Not in Library2 books Sutanu Sarkar, 2 books R. R. Mankbadi, 2 books V. A. Gushchin, 1 book R. Friedrich, 1 book IUTAM Symposium ( Palaiseau, France), 1 book.Close Drawer Menu Close Drawer Menu Menu.

Home; Journals. AIAA Journal; Journal of Aerospace Information Systems; Journal of Air Transportation; Journal of Aircraft; Journal of .A study was made of the wall pressure fluctuations in the reattachment region of a supersonic free shear layer. The free shear layer was formed by the separation of a Mach turbulent boundary.