A theoretical examination of the slotted-wall flow field is conducted to determine the appropriate wall pressure drop (or boundary condition) equation. This analysis improves the understanding of the fluid physics of these types of flow fields and helps in evaluating the uncertainties and limitations existing in previous mathematical developments. It is shown that the resulting slotted-wall boundary condition contains contributions from the airfoil-induced streamline curvature and the non-linear, quadratic, slot crossflow in addition to an often neglected linear term which results from viscous shearing in the slot. Existing and newly acquired experimental data are examined in the light of this formulation and theoretical developments
This paper presents results from an exploratory two-year effort of applying Computational Fluid Dyna...
A combined experimental-theoretical approach is developed for determination of the crossflow charact...
The paper describes a numerical study of the high-speed leg of the NASA Langley 14 x 22-ft Low-Speed...
The results of detailed parametric experiments are presented for the near-wall flow field of a longi...
A discussion of the flow field measurements obtained in the vertical plane at several stations along...
A method for analyzing wall interference is described which avoids the assumption of linear superpos...
The classic slotted-wall boundary-condition coefficient for rod-wall wind tunnels is derived by appr...
An airfoil design program and a boundary layer analysis were developed. Boundary conditions were der...
A procedure for designing slotted walls for two dimensional wind tunnels is is presented. The design...
A simplified physical model was constructed which simulates the viscous crossflow in a fluid layer n...
A large wind tunnel, approximately 8 feet in diameter, has been converted to transonic operation by ...
ABSTRACT: Transonic wind tunnels (TWT) are sophisticated tools for the investigations of flows with ...
ABSTRACT: Transonic wind tunnels (TWT) are sophisticated tools for the investigations of flows with ...
The paper describes the numerical study of the high-speed leg of the NASA Langley 14 by 22-foot Low ...
ABSTRACT: Transonic wind tunnels (TWT) are sophisticated tools for the investigations of flows with ...
This paper presents results from an exploratory two-year effort of applying Computational Fluid Dyna...
A combined experimental-theoretical approach is developed for determination of the crossflow charact...
The paper describes a numerical study of the high-speed leg of the NASA Langley 14 x 22-ft Low-Speed...
The results of detailed parametric experiments are presented for the near-wall flow field of a longi...
A discussion of the flow field measurements obtained in the vertical plane at several stations along...
A method for analyzing wall interference is described which avoids the assumption of linear superpos...
The classic slotted-wall boundary-condition coefficient for rod-wall wind tunnels is derived by appr...
An airfoil design program and a boundary layer analysis were developed. Boundary conditions were der...
A procedure for designing slotted walls for two dimensional wind tunnels is is presented. The design...
A simplified physical model was constructed which simulates the viscous crossflow in a fluid layer n...
A large wind tunnel, approximately 8 feet in diameter, has been converted to transonic operation by ...
ABSTRACT: Transonic wind tunnels (TWT) are sophisticated tools for the investigations of flows with ...
ABSTRACT: Transonic wind tunnels (TWT) are sophisticated tools for the investigations of flows with ...
The paper describes the numerical study of the high-speed leg of the NASA Langley 14 by 22-foot Low ...
ABSTRACT: Transonic wind tunnels (TWT) are sophisticated tools for the investigations of flows with ...
This paper presents results from an exploratory two-year effort of applying Computational Fluid Dyna...
A combined experimental-theoretical approach is developed for determination of the crossflow charact...
The paper describes a numerical study of the high-speed leg of the NASA Langley 14 x 22-ft Low-Speed...