Author: Valter J. E. StarkPublisher:
ISBN:
Category : Airplane wings
Languages : en
Pages : 32
Book Description
Calculation of Lifting Forces on Oscillating Wings
Author: Valter J. E. StarkPublisher:
ISBN:
Category : Airplane wings
Languages : en
Pages : 32
Book Description
Calculation of Lifting Forces on Oscillating Wings/ Valter J. E. Stark
Author: Valter J. E. StarkThe 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
The Calculation of Generalized Forces on Oscillating Wings in Supersonic Flow by Lifting Surface Theory
Author: G. Z. HarrisCalculation of Unsteady Transonic Aerodynamics for Oscillating Wings with Thickness
Author: S. Y. RuoPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 60
Book Description
An analytical approach is presented to account for some of the nonlinear characteristics of the transonic flow equation for finite thickness wings undergoing harmonic oscillation at sonic flight speed in an inviscid, shock-free fluid. The thickness effect is accounted for in the analysis through use of the steady local Mach number distribution over the wing at its mean position by employing the local linearization concept and a coordinate transformation. Computed results are compared with that of the linearized theory and experiments. Based on the local linearization concept, an alternate formulation avoiding the limitations of the coordinate transformation method is presented.
Calculation of Aerodynamic Forces on Slowly Oscillating Rectangular Wings in Subsonic Flow
Author: Netherlands. National Luchtvaart-LaboratoriumPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Downwash Tables for the Calculation of Aerodynamic Forces on Oscillating Wings
Author: Großbritannien Aeronautical Research CouncilPublisher:
ISBN:
Category : Downwash (Aerodynamics)
Languages : en
Pages : 174
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.
Author: