Significant aerodynamic interference can occur between high-speed bodies in close proximity. A complex flowfield develops where shock and expansion waves from a generator body impinge upon the adjacent receiver body. The pressure and flow angularity changes which occur across these disturbances modify the body aerodynamics. The aim of this research is to quantify the aerodynamic interference effects for multi-body configurations and understand the relevant flow physics. The interference aerodynamics for slender bodies in a supersonic flow were investigated through a parametric wind tunnel study. The receiver bodies were finned and un-finned configurations. The effect of lateral and axial body separations, receiver incidence and the strength...
An experimental study of the flow caused by a planar shock wave impinging obliquely on a cylinder is...
A wind tunnel investigation was conducted in which independent, steady state aerodynamic forces and ...
This research project aims at obtaining a better understanding of vertically translating the wing an...
Significant aerodynamic interference can occur between high-speed bodies in close proximity. A compl...
Aerodynamic interference can occur between high-speed bodies when in close proximity. A complex flo...
Aerodynamic interference can occur between high-speed slender bodies when in close proximity. A comp...
When two slender bodies are closely spaced within a supersonic freestream, substantial aerodynamic ...
An experimental investigation has been made into the interference effects present between three clos...
Some of the significant interference fields that may affect stability of aircraft at supersonic spee...
An experimental investigation was performed to determine the effect on base and forebody pressures o...
A description of the experimental investigation of the aerodynamic characteristics of variable geome...
A combined computational and experimental analysis was performed on a tangent ogive body with very l...
The turbulent flow of rotational bodies up to a length of 20 diameters with various head shapes and ...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
A combined experimental and analytical study was conducted to determine the relative magnitude of th...
An experimental study of the flow caused by a planar shock wave impinging obliquely on a cylinder is...
A wind tunnel investigation was conducted in which independent, steady state aerodynamic forces and ...
This research project aims at obtaining a better understanding of vertically translating the wing an...
Significant aerodynamic interference can occur between high-speed bodies in close proximity. A compl...
Aerodynamic interference can occur between high-speed bodies when in close proximity. A complex flo...
Aerodynamic interference can occur between high-speed slender bodies when in close proximity. A comp...
When two slender bodies are closely spaced within a supersonic freestream, substantial aerodynamic ...
An experimental investigation has been made into the interference effects present between three clos...
Some of the significant interference fields that may affect stability of aircraft at supersonic spee...
An experimental investigation was performed to determine the effect on base and forebody pressures o...
A description of the experimental investigation of the aerodynamic characteristics of variable geome...
A combined computational and experimental analysis was performed on a tangent ogive body with very l...
The turbulent flow of rotational bodies up to a length of 20 diameters with various head shapes and ...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
A combined experimental and analytical study was conducted to determine the relative magnitude of th...
An experimental study of the flow caused by a planar shock wave impinging obliquely on a cylinder is...
A wind tunnel investigation was conducted in which independent, steady state aerodynamic forces and ...
This research project aims at obtaining a better understanding of vertically translating the wing an...