A series of wind tunnel investigations were conducted to determine the flow characteristics downstream of a set of wind tunnel inlet flow conditioning vanes. The purpose was to develop an understanding of the flow mechanisms that contributed to the pressure loss and turbulence generated by the vane set. The near-field characteristics and flow field development were investigated with a 1/3 scale two dimensional model of the vane set at near full-scale Reynolds numbers. In a second series of tests, the global flow field characteristics were investigated by means of a 1/15 scale model of the full vane set and the 5:1 contraction leading to the model's test section. Scale effects due to Reynolds number mismatch were identified and their signifi...
Low-contraction ratio wind tunnel inlets have been shown to generate nonuniform velocity fields in t...
An experimental study directed at finding a deflector ramp that will reduce to an acceptable level t...
Rehabilitation of the Altitude Wind Tunnel includes the need for new corner turning vanes to match i...
The design and testing of vane sets and air-exchange inlet for the 40 x 80/80 x 120-ft wind tunnel a...
The aerodynamic characteristics of the 40- by 80-Foot Wind Tunnel at Ames Research Center were measu...
A 1/50th scale model of the 80- by 120-Foot Wind Tunnel (hereafter referred to as the 80x120) was ut...
Engineering: 3rd Place (The Ohio State University Denman Undergraduate Research Forum)The National F...
Detailed flow surveys downstream of the corner turning vanes and downstream of the fan inlet guide v...
The effect of the external wind on the quality of the flow in the test section was studied. The flow...
The features of a 1/50-scale model of the National Full-Scale Aerodynamics Complex are first describ...
The results of a series of flow quality and performance tests on several inlet and exit configuratio...
Two turning vane designs were experimentally evaluated for the fan-drive corner (corner 2) coupled t...
Two turning vane designs were experimentally evaluated for corner 2 of a 0.1 scale model of the NASA...
The present inlet design concept for an indraft wind tunnel, which is especially suited to applicati...
The study to develop inlet and exit treatments which would minimize the effect of external wind on t...
Low-contraction ratio wind tunnel inlets have been shown to generate nonuniform velocity fields in t...
An experimental study directed at finding a deflector ramp that will reduce to an acceptable level t...
Rehabilitation of the Altitude Wind Tunnel includes the need for new corner turning vanes to match i...
The design and testing of vane sets and air-exchange inlet for the 40 x 80/80 x 120-ft wind tunnel a...
The aerodynamic characteristics of the 40- by 80-Foot Wind Tunnel at Ames Research Center were measu...
A 1/50th scale model of the 80- by 120-Foot Wind Tunnel (hereafter referred to as the 80x120) was ut...
Engineering: 3rd Place (The Ohio State University Denman Undergraduate Research Forum)The National F...
Detailed flow surveys downstream of the corner turning vanes and downstream of the fan inlet guide v...
The effect of the external wind on the quality of the flow in the test section was studied. The flow...
The features of a 1/50-scale model of the National Full-Scale Aerodynamics Complex are first describ...
The results of a series of flow quality and performance tests on several inlet and exit configuratio...
Two turning vane designs were experimentally evaluated for the fan-drive corner (corner 2) coupled t...
Two turning vane designs were experimentally evaluated for corner 2 of a 0.1 scale model of the NASA...
The present inlet design concept for an indraft wind tunnel, which is especially suited to applicati...
The study to develop inlet and exit treatments which would minimize the effect of external wind on t...
Low-contraction ratio wind tunnel inlets have been shown to generate nonuniform velocity fields in t...
An experimental study directed at finding a deflector ramp that will reduce to an acceptable level t...
Rehabilitation of the Altitude Wind Tunnel includes the need for new corner turning vanes to match i...