The effect of front-to-rear propeller spacing on the interaction noise of a counterrotation propeller model was measured at cruise conditions. The data taken at an axial Mach number of 0.80 behaved as expected: interaction noise was reduced with increased spacing. The data taken at M=0.76 and M=0.72 did not behave as expected. At some of the test conditions the noise was unchanged; others even showed noise increases with increased spacing. A possible explanation, involving the amount of downstream blade area impacted by the tip vortex, is presented
A single rotation model propeller (SR-7A) was tested at simulated takeoff/approach conditions (Mach ...
The noise effect of operating supersonic tip speed propellers at angle of attack with respect to the...
A model high-speed, advanced counterrotation propeller, F7/A7, was tested in the anechoic wind tunne...
The noise of a counterrotation propeller at angle of attack was measured in the NASA Lewis 8- by 6-F...
A model high-speed advanced counterrotation propeller, F7/A3, was tested in the NASA Lewis Research ...
A scale model of a counterrotating propeller with forward-swept blades in the forward rotor and aft-...
Advanced counter-rotation propellers have been indicated as possibly generating an unacceptable amou...
Two modern high-speed advanced counterrotation propellers, F7/A7 and F7/A3 were tested in the NASA L...
The SR-7A propeller was acoustically tested with and without downstream swirl recovery vanes to dete...
Noise data on the Large-scale Advanced Propfan (LAP) propeller model SR-7A were taken in the NASA Le...
The effect of flight on blade surface pressures and propeller noise was reported. There were signifi...
Noise data on the SR-2 model propeller were taken in the NASA Lewis Research Center 8- by 6-Foot Win...
Performance data of 0.17-scale model counterrotation pusher propeller configurations were taken in t...
Detailed noise measurements were taken on the SR-7A propeller to investigate the behavior of the noi...
Acoustic and aerodynamic research at NASA Lewis Research Center on advanced propellers is reviewed i...
A single rotation model propeller (SR-7A) was tested at simulated takeoff/approach conditions (Mach ...
The noise effect of operating supersonic tip speed propellers at angle of attack with respect to the...
A model high-speed, advanced counterrotation propeller, F7/A7, was tested in the anechoic wind tunne...
The noise of a counterrotation propeller at angle of attack was measured in the NASA Lewis 8- by 6-F...
A model high-speed advanced counterrotation propeller, F7/A3, was tested in the NASA Lewis Research ...
A scale model of a counterrotating propeller with forward-swept blades in the forward rotor and aft-...
Advanced counter-rotation propellers have been indicated as possibly generating an unacceptable amou...
Two modern high-speed advanced counterrotation propellers, F7/A7 and F7/A3 were tested in the NASA L...
The SR-7A propeller was acoustically tested with and without downstream swirl recovery vanes to dete...
Noise data on the Large-scale Advanced Propfan (LAP) propeller model SR-7A were taken in the NASA Le...
The effect of flight on blade surface pressures and propeller noise was reported. There were signifi...
Noise data on the SR-2 model propeller were taken in the NASA Lewis Research Center 8- by 6-Foot Win...
Performance data of 0.17-scale model counterrotation pusher propeller configurations were taken in t...
Detailed noise measurements were taken on the SR-7A propeller to investigate the behavior of the noi...
Acoustic and aerodynamic research at NASA Lewis Research Center on advanced propellers is reviewed i...
A single rotation model propeller (SR-7A) was tested at simulated takeoff/approach conditions (Mach ...
The noise effect of operating supersonic tip speed propellers at angle of attack with respect to the...
A model high-speed, advanced counterrotation propeller, F7/A7, was tested in the anechoic wind tunne...