Author: Hideo Yoshihara
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
Book Description
Planar Inviscid Transonic Airfoil Theory
Some Recent Developments in Planar Inviscid Transonic Airfoil Theory
Author: Hideo Yoshihara
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 52
Book Description
Some Recent Developments in Planar Inviscid Transonic Airfoil Theory
Steady Inviscid Transonic Flows Over Planar Airfoils
Author: R. Magnus
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 68
Book Description
A finite difference procedure based upon a system of unsteady equations in proper conservation form with either exact or small disturbance steady terms is used to calculate the steady flows over several classes of airfoils. The airfoil condition is fulfilled on a slab whose upstream extremity is a semi-circle overlaying the airfoil leading edge circle. The limitations of the small disturbance equations are demonstrated in an extreme example of a blunt-nosed, aft-cambered airfoil. The necessity of using the equations in proper conservation form to capture the shock properly is stressed. Ability of the steady relaxation procedures to capture the shock is briefly examined.
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 68
Book Description
A finite difference procedure based upon a system of unsteady equations in proper conservation form with either exact or small disturbance steady terms is used to calculate the steady flows over several classes of airfoils. The airfoil condition is fulfilled on a slab whose upstream extremity is a semi-circle overlaying the airfoil leading edge circle. The limitations of the small disturbance equations are demonstrated in an extreme example of a blunt-nosed, aft-cambered airfoil. The necessity of using the equations in proper conservation form to capture the shock properly is stressed. Ability of the steady relaxation procedures to capture the shock is briefly examined.
An Inviscid Analysis of Transonic, Slatted Airfoils
Author: David A. Caughey
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 24
Book Description
An Improved Viscid/inviscid Interaction Procedure for Transonic Flow Over Airfoils
Author: R. E. Melnik
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 144
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 144
Book Description
Application of Linearized Transonic Theory to Tunnel Blockage Interference
Author: C. F. Lo
Publisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 34
Book Description
Publisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 34
Book Description
An Improved Viscid/inviscid Interaction Procedure for Transonic Flow Over Airfoils
Author:
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 144
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 144
Book Description
Some Recent Developments in Planar Inviscid Airfoil Theory
An Analysis of the Inviscid Transonic Flow Over Two-Element Airfoil Systems
Author: B. Grossman
Publisher:
ISBN:
Category :
Languages : en
Pages : 51
Book Description
This report describes the development of a method for numerically computing the inviscid transonic flow field over an airfoil with a leading-edge slat or a trailing-edge flap. The approach is to solve the full inviscid irrotational flow equations about two-element airfoil systems. The methodology consists of the development of a suitable computational plane and grid system through the application of a series of conformal mappings. The appropriate set of equations and boundary conditions are derived in terms of a smoothly varying, single-valued reduced potential function through analytic removal of all singularities in the computational domain. A stable and accurate relaxation procedure is established for the numerical solution of the governing equations. The method is applied to a variety of transonic supercritical two-element airfoil configurations. Results are presented depicting the surface pressure distribution, streamline patterns in the physical and computational domain, and Mach number contours. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 51
Book Description
This report describes the development of a method for numerically computing the inviscid transonic flow field over an airfoil with a leading-edge slat or a trailing-edge flap. The approach is to solve the full inviscid irrotational flow equations about two-element airfoil systems. The methodology consists of the development of a suitable computational plane and grid system through the application of a series of conformal mappings. The appropriate set of equations and boundary conditions are derived in terms of a smoothly varying, single-valued reduced potential function through analytic removal of all singularities in the computational domain. A stable and accurate relaxation procedure is established for the numerical solution of the governing equations. The method is applied to a variety of transonic supercritical two-element airfoil configurations. Results are presented depicting the surface pressure distribution, streamline patterns in the physical and computational domain, and Mach number contours. (Author).