Author: Hideo Yoshihara
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 52
Book Description
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
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 958
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 958
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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.
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
Scientific and Technical Aerospace Reports
AIAA 73-622 - AIAA 73-658
AGARD Report
AGARD Bulletin
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 752
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 752
Book Description
Advances in Numerical Fluid Dynamics
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 162
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 162
Book Description