Author: G. Z. HarrisPublisher:
ISBN:
Category :
Languages : en
Pages : 43
Book Description
The Calculation of Generalized Forces on Oscillating Wings in Supersonic Flow by Lifting Surface Theory
Author: G. Z. HarrisThe Calculation of Generalised Forces on Oscillating Wings in Supersonic Flow by Lifting Surface Theory
Author: Aeronautical Research Council (Great Britain)Publisher:
ISBN:
Category :
Languages : en
Pages : 43
Book Description
The Calculation of Generalised Forces on Oscillating Wings in Supersonic Flow by Lifting Surface Theory
Author: G. Z. HarrisPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 43
Book Description
Theoretical Study of Air Forces on an Oscillating Or Steady Thin Wing in a Supersonic Main Stream
Author: Isadore Edward GarrickPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 50
Book Description
This paper constitutes a theoretical study of the aerodynamic forces on an oscillating or steady wing of finite span moving forward at a uniform supersonic speed. The treatment is based on the linearized theory obtained by considering only small disturbances in an ideal fluid. The wing is therefore considered to be a nearly flat thin surface at a small angle of attack and the flow is considered non- viscous and free of strong shocks. The theory in this case is equivalent to finding certain solutions of the wave equation in three dimensions with respect to a moving coordinate system.
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 960
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.
Measurement of Aerodynamic Forces on an Oscillating Airfoil
Author: Richard I. WindsorPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 252
Book Description
A literature survey was conducted to determine the state of the art of measuring and predicting aerodynamic characteristics of oscillating air-foils. Aerodynamic forces on a two-dimensional NACA 0012 airfoil oscillating sinusoidally in pitch were measured by two techniques. The forces were obtained from pressure measurements and by means of strain gage balances. Pressure measurements were made on the airfoil oscillating in pitch about the quarter-chord point at various mean angles of attack. Strain gage balance readings were obtained for models with pitch axis located at 25, 37, and 50 percent chord points oscillating about various mean angles. Direct force measurements were employed in an effort to obtain drag data. Instantaneous pressure distributions are presneted for representative oscillating conditions. (Author).
A Method for Calculating the Generalized Aerodynamic Forces on Rectangular Wings Deforming Symmetrically in Supersonic Flight with Indicial Or Sinusoidal Time Dependence
Author: Technical Abstract Bulletin
Author: NASA Technical Note
Author: Two-dimensional Wing Theory in the Supersonic Range
Author: H. HönlPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 764
Book Description
The plane problem of the vibrating airfoil in supersonic flow is dealt with and solved within the scope of a linearized theory by the method of the acceleration potential.