Author: Shahyar PirzadehPublisher:
ISBN:
Category :
Languages : en
Pages : 114
Book Description
Three-dimensional unsteady transonic viscous-inviscid interaction
Author: Shahyar PirzadehCalculation of Unsteady Transonic Flows with Mild Separation by Viscous-inviscid Interaction
Author: James T. HowlettPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 44
Book Description
Calculation of Unsteady Transonic Flows with Mild Separation by Viscous-inviscid Interaction
Author: James T. HowlettUnsteady Viscous-inviscid Interaction Procedures for Transonic Airfoil Flows
Author: Tracy DoneganPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 60
Book Description
Numerical Solution of Three-dimensional Unsteady Transonic Flow Over Wings Including Inviscid/viscous Interactions
Author: Calculation of Unsteady Transonic Flows with Mild Separation by Viscous-Inviscid Interaction
Author: National Aeronautics and Space Adm NasaPublisher:
ISBN: 9781729430842
Category :
Languages : en
Pages : 44
Book Description
This paper presents a method for calculating viscous effects in two- and three-dimensional unsteady transonic flow fields. An integral boundary-layer method for turbulent viscous flow is coupled with the transonic small-disturbance potential equation in a quasi-steady manner. The viscous effects are modeled with Green's lag-entrainment equations for attached flow and an inverse boundary-layer method for flows that involve mild separation. The boundary-layer method is used stripwise to approximate three-dimensional effects. Applications are given for two-dimensional airfoils, aileron buzz, and a wing planform. Comparisons with inviscid calculations, other viscous calculation methods, and experimental data are presented. The results demonstrate that the present technique can economically and accurately calculate unsteady transonic flow fields that have viscous-inviscid interactions with mild flow separation. Howlett, James T. Langley Research Center RTOP 509-10-02-03...
Unsteady Viscous-Inviscid Interaction Procedures for Transonic Airfoil Flows
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This study is concerned with the development of a computational algorithm for viscous-inviscid interactions with application to two-dimensional transonic airfoil flows. The inner viscous flow is computed by the integral method of Whitfield, while the external flow is calculated by Jameson's Euler equation code. The two flows are matched by a linearized boundary condition at the airfoil surface. Of particular interest is the use of a time-dependent boundary-layer calculation method since it has been determined that a time-dependent method is desirable for extending the interaction method to three-dimensional flows. In general, it is found that the agreement between theoretical prediction and experimental data is satisfactory for engineering calculations.
Unsteady Viscous-Inviscid Interaction Procedures for Transonic Airfoil Flows
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This study is concerned with the development of a computational algorithm for viscous-inviscid interactions with application to two-dimensional transonic airfoil flows. The inner viscous flow is computed by the integral method of Whitfield, while the external flow is calculated by Jameson's Euler equation code. The two flows are matched by a linearized boundary condition at the airfoil surface. Of particular interest is the use of a time-dependent boundary-layer calculation method since it has been determined that a time-dependent method is desirable for extending the interaction method to three-dimensional flows. In general, it is found that the agreement between theoretical prediction and experimental data is satisfactory for engineering calculations.
Computation of Viscous Phenomena in Unsteady Transonic Flow
Author: U. R. MullerPublisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
Progress in the development towards a 30 viscous-inviscid strong interaction method for computing unsteady transonic wing flow is reported. In the current version, an ADI-technique for solving the 3D unsteady Transonic Small Perturbation Equation (TSP) has been extended by incorporating an unsteady 2D integral boundary layer method and then simultaneously solving the viscous and inviscid flow equations in a stripwise fashion.
Author: