A theoretical method is presented for calculating the flow field about wing-body combinations employing bodies deviating only slightly in shape from a circular cylinder. The method is applied to the calculation of the pressure field acting between a circular cylindrical body and a rectangular wing. The case of zero body angle of attack and variable wing incidence is considered as well as the case of zero wing incidence and variable body angle of attack. An experiment was performed especially for the purpose of checking the calculative examples
Two different singularity methods have been utilized to calculate the potential flow past a three di...
The aerodynamic forces on bodies of arbitrary shape were investigated under conditions such that the...
Pressure distributions are calculated for some symmetrical wing-body combinations at zero lift. The ...
A theoretical method is presented for calculating the flow field about wing-body combinations employ...
In order to investigate the effects of drag interference on wing-body combinations, tests were condu...
The wing-body interference theory of NACA TN 2677 applied to symmetrical wings in combination with q...
The theoretical lift of a cylindrical afterbody at zero angle of attack due to incidence of the wing...
This report describes a theoretical method for estimating the aerodynamic loading on a wing-body con...
The wave drag of a combination of slender bodies of revolution at zero angle of attack is studied wi...
Fluid body interaction is a phenomenon that is simple to observe, but very complicated to understand...
A method of analysis based on slender-wing theory is developed to investigate the characteristics in...
Numerical results concerning wing-body interference for compressible flow obtained by the use of an ...
A new method has been developed for calculating the pressure distribution and aerodynamic characteri...
The objective of this paper is to describe theoretical procedures which can be utilized by the gener...
The present thesis is aimed at investigating the effect of small angles of attack on the flow around...
Two different singularity methods have been utilized to calculate the potential flow past a three di...
The aerodynamic forces on bodies of arbitrary shape were investigated under conditions such that the...
Pressure distributions are calculated for some symmetrical wing-body combinations at zero lift. The ...
A theoretical method is presented for calculating the flow field about wing-body combinations employ...
In order to investigate the effects of drag interference on wing-body combinations, tests were condu...
The wing-body interference theory of NACA TN 2677 applied to symmetrical wings in combination with q...
The theoretical lift of a cylindrical afterbody at zero angle of attack due to incidence of the wing...
This report describes a theoretical method for estimating the aerodynamic loading on a wing-body con...
The wave drag of a combination of slender bodies of revolution at zero angle of attack is studied wi...
Fluid body interaction is a phenomenon that is simple to observe, but very complicated to understand...
A method of analysis based on slender-wing theory is developed to investigate the characteristics in...
Numerical results concerning wing-body interference for compressible flow obtained by the use of an ...
A new method has been developed for calculating the pressure distribution and aerodynamic characteri...
The objective of this paper is to describe theoretical procedures which can be utilized by the gener...
The present thesis is aimed at investigating the effect of small angles of attack on the flow around...
Two different singularity methods have been utilized to calculate the potential flow past a three di...
The aerodynamic forces on bodies of arbitrary shape were investigated under conditions such that the...
Pressure distributions are calculated for some symmetrical wing-body combinations at zero lift. The ...