A preliminary study of the exhaust flow from the Ames Research Center 80 by 120 Foot Wind Tunnel indicated that the flow might pose a hazard to low-flying light aircraft operating in the Moffett Field traffic pattern. A more extensive evaluation of the potential hazard was undertaken using a fixed-base, piloted simulation of a light, twin-engine, general-aviation aircraft. The simulated aircraft was flown through a model of the wind tunnel exhaust by pilots of varying experience levels to develop a data base of aircraft and pilot reactions. It is shown that a light aircraft would be subjected to a severe disturbance which, depending upon entry condition and pilot reaction, could result in a low-altitude stall or cause damage to the aircraft...
The paper describes the numerical study of the high-speed leg of the NASA Langley 14 by 22-foot Low ...
A wind tunnel investigation of the windstream-engine exhaust flow interaction on a light observation...
Much remains to be learned about the hazards of low altitude wind shear to aviation. New research sh...
An experimental study directed at finding a deflector ramp that will reduce to an acceptable level t...
Aeronautical applications of simulation technology at Ames Research Center are described. The larges...
Experiments were carried out in a small wind tunnel in which atmospheric flow around buildings was s...
Measurements of longitudinal mean velocity and turbulence intensity were made in the wake of a recta...
A series of wind tunnel tests were conducted to assess the effects of leading edge ice contamination...
The aerodynamic characteristics of the 40- by 80-Foot Wind Tunnel at Ames Research Center were measu...
A two part study was conducted to determine the feasibility of predicting the conditions under which...
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...
Nacelle induced flutter effects in elastodynamic scaled model of fan jet transport aircraft mounted ...
Manned flight simulator response to theoretical wind shear profiles was studied in an effort to cali...
A 1/50th scale model of the 80- by 120-Foot Wind Tunnel (hereafter referred to as the 80x120) was ut...
The paper describes the numerical study of the high-speed leg of the NASA Langley 14 by 22-foot Low ...
A wind tunnel investigation of the windstream-engine exhaust flow interaction on a light observation...
Much remains to be learned about the hazards of low altitude wind shear to aviation. New research sh...
An experimental study directed at finding a deflector ramp that will reduce to an acceptable level t...
Aeronautical applications of simulation technology at Ames Research Center are described. The larges...
Experiments were carried out in a small wind tunnel in which atmospheric flow around buildings was s...
Measurements of longitudinal mean velocity and turbulence intensity were made in the wake of a recta...
A series of wind tunnel tests were conducted to assess the effects of leading edge ice contamination...
The aerodynamic characteristics of the 40- by 80-Foot Wind Tunnel at Ames Research Center were measu...
A two part study was conducted to determine the feasibility of predicting the conditions under which...
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...
Nacelle induced flutter effects in elastodynamic scaled model of fan jet transport aircraft mounted ...
Manned flight simulator response to theoretical wind shear profiles was studied in an effort to cali...
A 1/50th scale model of the 80- by 120-Foot Wind Tunnel (hereafter referred to as the 80x120) was ut...
The paper describes the numerical study of the high-speed leg of the NASA Langley 14 by 22-foot Low ...
A wind tunnel investigation of the windstream-engine exhaust flow interaction on a light observation...
Much remains to be learned about the hazards of low altitude wind shear to aviation. New research sh...