The flow field between a model empennage and a 591-mm-diameter pusher propeller was studied in the Ames 7- by 10-Foot Wind Tunnel with directional pressure probes and hot-wire anemometers. The region probed was bounded by the empennage trailing edge and downstream propeller. The wake properties, including effects of propeller operation on the empennage wake, were investigated for two empennage geometries: one, a vertical tail fin, the other, a Y-tail with a 34 deg dihedral. Results showed that the effect of the propeller on the empennage wake upstream of the propeller was not strong. The flow upstream of the propeller was accelerated in the streamwise direction by the propeller, but the empennage wake width and velocity defect were relative...
A model was designed, fabricated and wind tunnel tested to identify some of the parameters which wer...
This paper presents a comprehensive experimental aeroacoustic investigation of a propeller under tur...
Finite element theory is used to calculate the acoustic field of a propeller in a soft walled circul...
In the present study an experimental analysis of the velocity and pressure fields behind a marine pr...
Open rotors are considered to have the potential to improve the fuel economy of aircraft significant...
Acoustic and aerodynamic research at NASA Lewis Research Center on advanced propellers is reviewed i...
In the present study an experimental analysis of the velocity and pressure fields behind a marine pr...
Pylon trailing edge blowing was investigated as a means of alleviating the effects of the pylon wake...
Advanced propeller propulsion systems potentially provide a significant reduction in fuel burn compa...
This paper presents an experimental assessment of the working principles of pylon trailing-edge blow...
Advanced propellers promise significant fuel-burn savings compared to turbofans. When installed on t...
A scale model of a counterrotating propeller with forward-swept blades in the forward rotor and aft-...
Results are presented of an investigation to measure the flowfield generated by an advanced counterr...
The effect of flight on blade surface pressures and propeller noise was reported. There were signifi...
Recent results of aerodynamic and acoustic research on both single rotation and counterrotation prop...
A model was designed, fabricated and wind tunnel tested to identify some of the parameters which wer...
This paper presents a comprehensive experimental aeroacoustic investigation of a propeller under tur...
Finite element theory is used to calculate the acoustic field of a propeller in a soft walled circul...
In the present study an experimental analysis of the velocity and pressure fields behind a marine pr...
Open rotors are considered to have the potential to improve the fuel economy of aircraft significant...
Acoustic and aerodynamic research at NASA Lewis Research Center on advanced propellers is reviewed i...
In the present study an experimental analysis of the velocity and pressure fields behind a marine pr...
Pylon trailing edge blowing was investigated as a means of alleviating the effects of the pylon wake...
Advanced propeller propulsion systems potentially provide a significant reduction in fuel burn compa...
This paper presents an experimental assessment of the working principles of pylon trailing-edge blow...
Advanced propellers promise significant fuel-burn savings compared to turbofans. When installed on t...
A scale model of a counterrotating propeller with forward-swept blades in the forward rotor and aft-...
Results are presented of an investigation to measure the flowfield generated by an advanced counterr...
The effect of flight on blade surface pressures and propeller noise was reported. There were signifi...
Recent results of aerodynamic and acoustic research on both single rotation and counterrotation prop...
A model was designed, fabricated and wind tunnel tested to identify some of the parameters which wer...
This paper presents a comprehensive experimental aeroacoustic investigation of a propeller under tur...
Finite element theory is used to calculate the acoustic field of a propeller in a soft walled circul...