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Planar Inviscid Transonic Airfoil Theory

Planar Inviscid Transonic Airfoil Theory PDF Author: Hideo Yoshihara
Publisher:
ISBN:
Category :
Languages : en
Pages : 33

Book Description


Planar Inviscid Transonic Airfoil Theory

Planar Inviscid Transonic Airfoil Theory PDF Author: Hideo Yoshihara
Publisher:
ISBN:
Category :
Languages : en
Pages : 33

Book Description


Some Recent Developments in Planar Inviscid Transonic Airfoil Theory

Some Recent Developments in Planar Inviscid Transonic Airfoil Theory PDF Author: Hideo Yoshihara
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 52

Book Description


Some Recent Developments in Planar Inviscid Transonic Airfoil Theory

Some Recent Developments in Planar Inviscid Transonic Airfoil Theory PDF Author: Hideo Yoshihara
Publisher:
ISBN:
Category :
Languages : en
Pages : 33

Book Description


Steady Inviscid Transonic Flows Over Planar Airfoils

Steady Inviscid Transonic Flows Over Planar Airfoils PDF 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.

An Inviscid Analysis of Transonic, Slatted Airfoils

An Inviscid Analysis of Transonic, Slatted Airfoils PDF Author: David A. Caughey
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 24

Book Description


An Improved Viscid/inviscid Interaction Procedure for Transonic Flow Over Airfoils

An Improved Viscid/inviscid Interaction Procedure for Transonic Flow Over Airfoils PDF Author: R. E. Melnik
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 144

Book Description


Application of Linearized Transonic Theory to Tunnel Blockage Interference

Application of Linearized Transonic Theory to Tunnel Blockage Interference PDF Author: C. F. Lo
Publisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 34

Book Description


An Improved Viscid/inviscid Interaction Procedure for Transonic Flow Over Airfoils

An Improved Viscid/inviscid Interaction Procedure for Transonic Flow Over Airfoils PDF Author:
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 144

Book Description


Some Recent Developments in Planar Inviscid Airfoil Theory

Some Recent Developments in Planar Inviscid Airfoil Theory PDF Author: Hideo Yoshihara
Publisher:
ISBN:
Category :
Languages : en
Pages : 33

Book Description


An Analysis of the Inviscid Transonic Flow Over Two-Element Airfoil Systems

An Analysis of the Inviscid Transonic Flow Over Two-Element Airfoil Systems PDF 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).