A 1/50th scale model of the 80- by 120-Foot Wind Tunnel (hereafter referred to as the 80x120) was utilized to determine the magnitude of turbulence caused by buildings located upstream of the wind tunnel inlet. The 1/50th scale models of existing and proposed buildings were constructed to act as blockage for the test. Various inlet locations were sampled for turbulence intensity levels under a variety of blockage conditions including simple three-dimensional rectangular bodies creating quasi two-dimensional physics along the tunnel centerline, existing building structures in the vicinity of the full-scale wind tunnel inlet flow field, and proposed building structures that may someday be constructed at NASA Ames Research Center upwind of the...
Prior to the NASA Glenn Research Center 9- by 15-Foot Low-Speed Wind Tunnel (9x15 LSWT) undergoing s...
An experimental study directed at finding a deflector ramp that will reduce to an acceptable level t...
A brief overview is given of the National Full-scale Aerodynamics Complex. Its geometry, design, con...
Engineering: 3rd Place (The Ohio State University Denman Undergraduate Research Forum)The National F...
A series of wind tunnel investigations were conducted to determine the flow characteristics downstre...
Measurements of longitudinal mean velocity and turbulence intensity were made in the wake of a recta...
The aerodynamic characteristics of the 40- by 80-Foot Wind Tunnel at Ames Research Center were measu...
Experiments were carried out in a small wind tunnel in which atmospheric flow around buildings was s...
The effect of the external wind on the quality of the flow in the test section was studied. The flow...
Detailed wind speed profile measurements were made in the wake of 1/25 scale and 1/48 scale tower mo...
The features of a 1/50-scale model of the National Full-Scale Aerodynamics Complex are first describ...
The design and testing of vane sets and air-exchange inlet for the 40 x 80/80 x 120-ft wind tunnel a...
The purpose of this report is to investigate the status and future projections for the question of s...
With the assistance and cooperation of the National Advisory Committee for Aeronautics the Bureau of...
A full-scale field study of the wind over a simulated two-dimensional building is reported. The stud...
Prior to the NASA Glenn Research Center 9- by 15-Foot Low-Speed Wind Tunnel (9x15 LSWT) undergoing s...
An experimental study directed at finding a deflector ramp that will reduce to an acceptable level t...
A brief overview is given of the National Full-scale Aerodynamics Complex. Its geometry, design, con...
Engineering: 3rd Place (The Ohio State University Denman Undergraduate Research Forum)The National F...
A series of wind tunnel investigations were conducted to determine the flow characteristics downstre...
Measurements of longitudinal mean velocity and turbulence intensity were made in the wake of a recta...
The aerodynamic characteristics of the 40- by 80-Foot Wind Tunnel at Ames Research Center were measu...
Experiments were carried out in a small wind tunnel in which atmospheric flow around buildings was s...
The effect of the external wind on the quality of the flow in the test section was studied. The flow...
Detailed wind speed profile measurements were made in the wake of 1/25 scale and 1/48 scale tower mo...
The features of a 1/50-scale model of the National Full-Scale Aerodynamics Complex are first describ...
The design and testing of vane sets and air-exchange inlet for the 40 x 80/80 x 120-ft wind tunnel a...
The purpose of this report is to investigate the status and future projections for the question of s...
With the assistance and cooperation of the National Advisory Committee for Aeronautics the Bureau of...
A full-scale field study of the wind over a simulated two-dimensional building is reported. The stud...
Prior to the NASA Glenn Research Center 9- by 15-Foot Low-Speed Wind Tunnel (9x15 LSWT) undergoing s...
An experimental study directed at finding a deflector ramp that will reduce to an acceptable level t...
A brief overview is given of the National Full-scale Aerodynamics Complex. Its geometry, design, con...