Results 111 to 120 of about 12,206 (226)

User's manual for UCAP: Unified Counter-Rotation Aero-Acoustics Program [PDF]

open access: yes
This is the user's manual for the Unified Counter-rotation Aeroacoustics Program (UCAP), the counter-rotation derivative of the UAAP (Unified Aero-Acoustic Program).
Culver, E. M., Mccolgan, C. J.
core   +1 more source

Aeroacoustics of advanced propellers [PDF]

open access: yes
The aeroacoustics of advanced, high speed propellers (propfans) are reviewed from the perspective of NASA research conducted in support of the Advanced Turboprop Program.
Groeneweg, John F.
core   +1 more source

Effect of boattail geometry on the acoustics of parallel baffles in ducts [PDF]

open access: yes
Sound attenuation and total pressure drop of parallel duct baffles incorporating certain boattail geometries were measured in the NASA Ames Research Center 7- by 10-Foot Wind Tunnel.
Dudley, M. R.   +2 more
core   +1 more source

Analytical simulation of the far-field jet noise and the unsteady jet flow-field by a model of periodic shedding of vortex ring from the jet exit [PDF]

open access: yes
The construction of a theoretical flow field due to shedding of vortex rings, the identification of the controlling parameters, and the determination of whether the theoretical model successfully simulated the unsteady pressure field near jet (and ...
Liu, C. H.
core   +1 more source

Reviews in Aeroacoustics [PDF]

open access: yesInternational Journal of Aeroacoustics, 2010
openaire   +1 more source

Simulation-Based Assessment of a Full-Scale Installed Quiet Landing Gear [PDF]

open access: yes
Full-scale simulations of a Gulfstream G-III aircraft, performed in support of the NASA Acoustic Research Measurements flights, are presented to complement results discussed in earlier studies.
Duda, Benjamin   +2 more
core   +1 more source

Unsteady-flow-field predictions for oscillating cascades [PDF]

open access: yes
The unsteady flow field around an oscillating cascade of flat plates with zero stagger was studied by using a time marching Euler code. This case had an exact solution based on linear theory and served as a model problem for studying pressure wave ...
Huff, Dennis L.
core   +1 more source

On the Use of Acoustic Wind Tunnel Data for the Simulation of sUAS Flyover Noise [PDF]

open access: yes
Acoustic measurements of a small, unmanned aerial system were recently acquired during a ground test campaign. The purposes of the ground test, conducted in the NASA Langley Low Speed Aeroacoustic Wind Tunnel, were to characterize the source noise in ...
Pettingill, Nicole A.   +2 more
core   +1 more source

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