Add to ORKGMeasures to reduce the intensity of fan noise in the NASA Langley 30 ft x 60 ft subsonic wind tunnel...
The applicability of the NASA Ames 40- by 80-ft wind tunnel for acoustic research on STOL concepts h...
A cooperative program between the Royal Aircraft Establishment (RAE), England, and the NASA Ames Res...
Measurements were made in the no. 1 7'x10' wind tunnel at NASA Ames Research Center, with the object...
The results are presented of the acoustical measurements made to supply NASA Langley operating perso...
The full-scale wind tunnel at NASA-Langley Research Center was designed for low-speed aerodynamic te...
The NASA Flight Effects Program has a requirement to compare acoustic data obtained from flyover, st...
The NASA LaRC 4 x 7 Meter Wind Tunnel is an existing facility specially designed for powered low spe...
Experimental evaluations of the acoustical characteristics and source sound power and directionality...
Based on exploratory acoustic measurements in Langley's V/STOL wind tunnel, recommendations are made...
The test section of the NASA Lewis 9- by 15-Foot Low Speed Wind Tunnel was acoustically treated to a...
Feasibility of model acoustic measurements in wind tunnel for estimating total sound powe
Acoustical characteristics and source directionality measurement capabilities of the wind tunnel in ...
The 9- by 15-Foot Low Speed Wind Tunnel has been used for acoustic testing for more than 40 years. T...
Methods are presented for making overall and directional acoustic measurements with forward velocity...
Measures to reduce the intensity of fan noise in the NASA Langley 30 ft x 60 ft subsonic wind tunnel...
The applicability of the NASA Ames 40- by 80-ft wind tunnel for acoustic research on STOL concepts h...
A cooperative program between the Royal Aircraft Establishment (RAE), England, and the NASA Ames Res...
Measurements were made in the no. 1 7'x10' wind tunnel at NASA Ames Research Center, with the object...
The results are presented of the acoustical measurements made to supply NASA Langley operating perso...
The full-scale wind tunnel at NASA-Langley Research Center was designed for low-speed aerodynamic te...
The NASA Flight Effects Program has a requirement to compare acoustic data obtained from flyover, st...
The NASA LaRC 4 x 7 Meter Wind Tunnel is an existing facility specially designed for powered low spe...
Experimental evaluations of the acoustical characteristics and source sound power and directionality...
Based on exploratory acoustic measurements in Langley's V/STOL wind tunnel, recommendations are made...
The test section of the NASA Lewis 9- by 15-Foot Low Speed Wind Tunnel was acoustically treated to a...
Feasibility of model acoustic measurements in wind tunnel for estimating total sound powe
Acoustical characteristics and source directionality measurement capabilities of the wind tunnel in ...
The 9- by 15-Foot Low Speed Wind Tunnel has been used for acoustic testing for more than 40 years. T...
Methods are presented for making overall and directional acoustic measurements with forward velocity...
Measures to reduce the intensity of fan noise in the NASA Langley 30 ft x 60 ft subsonic wind tunnel...
The applicability of the NASA Ames 40- by 80-ft wind tunnel for acoustic research on STOL concepts h...
A cooperative program between the Royal Aircraft Establishment (RAE), England, and the NASA Ames Res...