E-LIB Suche - Ergebnisse für: Proença, Anderson

1

Investigation into the turbulence statistics of installed j..:

Proença, Anderson ; Lawrence, Jack ; Self, Rod
Experiments in Fluids. 61 (2020) 10 - p. , 2020

Link: https://doi.org/10.1007/..

2

Measurements of the single-point and joint turbulence stati..:

Proença, Anderson ; Lawrence, Jack ; Self, Rod
Experiments in Fluids. 60 (2019) 4 - p. , 2019

Link: https://doi.org/10.1007/..

3

Toward Estimating Noise–Power–Distance Curves for Propeller..:

Amargianitakis, Daniel C. ; Self, Rodney H. ; Torija, Antonio J...
Journal of Aircraft. 61 (2024) 2 - p. 485-502 , 2024

Link: https://doi.org/10.2514/..

4

Closed-Form Analytical Approach for Calculating Noise Conto..:

Amargianitakis, Daniel C. ; Self, Rodney H. ; Synodinos, Athanasios P...
AIAA Journal. 61 (2023) 4 - p. 1735-1748 , 2023

Link: https://doi.org/10.2514/..

5

Jet Flow and Noise Predictions for the Doak Laboratory Expe..:

Gryazev, Vasily ; Markesteijn, Annabel P. ; Karabasov, Sergey A...
AIAA Journal. 61 (2023) 7 - p. 3078-3090 , 2023

Link: https://doi.org/10.2514/..

6

Experimental Flowfield Analyses of Installed Subsonic Jet–P..:

Proença, Anderson R. ; Lawrence, Jack L. T.
AIAA Journal. 60 (2022) 3 - p. 1630-1642 , 2022

Link: https://doi.org/10.2514/..

7

Evaluation of Turbulent Jet Characteristic Scales Using Joi..:

Proença, Anderson R. ; Meloni, Stefano
Fluids. 7 (2022) 4 - p. 125 , 2022

Link: https://doi.org/10.3390/..

8

An experimental investigation into model-scale installed je..:

Meloni, Stefano ; Proença, Anderson R. ; Lawrence, Jack L.T..
Journal of Fluid Mechanics. 929 (2021) - p. , 2021

Link: https://doi.org/10.1017/..

9

Wall pressure fluctuations induced by a single stream jet o..:

Meloni, Stefano ; Lawrence, Jack LT ; Proença, Anderson R..
International Journal of Aeroacoustics. 19 (2020) 3-5 - p. 240-253 , 2020

Link: https://doi.org/10.1177/..

10

Experimental characterization of velocity and acoustic fiel..:

de Almeida, Odenir ; Proença, Anderson Ramos ; Self, Rodney Harold
Applied Acoustics. 127 (2017) - p. 194-206 , 2017

Link: https://doi.org/10.1016/..

11

Reestruturação produtiva e consolidação de novos eixos de d..:

Proença, Anderson Dias de Almeida ; Santos Jr., Wilson Ribeiros dos
Revista Brasileira de Estudos Urbanos e Regionais. 21 (2019) 2 - p. 312 , 2019

Link: https://doi.org/10.22296..

12

Feasibility of a spinning cylinder on the leading and trail..:

Francannet, Antoine ; Prince, Simon A ; Di Pasquale, Davide.
Francannet A, Prince S, Di Pasquale D, Proenca A. (2023) Feasibility of a spinning cylinder on the leading and trailing edges of a flap for high lift. In: AIAA SciTech Forum 2023, 23-27 January 2023, National Harbor, Maryland, USA. Paper number AIAA 2023-0053. , 2023

Link: https://doi.org/10.2514/..

13

Upstream turbulence effects on the self-similarity of wakes..:

Murari, Prasanth K ; Proenca, Anderson ; Garry, Kevin P
Murari PK, Proenca A, Garry KP. (2023) Upstream turbulence effects on the self-similarity of wakes: vortex pair dynamics. In: AIAA SciTech Forum 2023, 23-27 January 2023, National Harbor, Maryland, USA. , 2023

Link: https://doi.org/10.2514/..

14

Analysis of triangular cross-section slender bodies in supe..:

Bourny, Quentin ; Proenca, Anderson ; Di Pasquale, Davide Di.
Bourny Q, Proença AR, Di Pasquale D, Prince SA. (2023) Analysis of triangular cross-section slender bodies in supersonic regime using RANS simulations. In: 2023 AIAA Aviation and Aeronautics Forum and Exposition (AIAA AVIATION Forum), 12-16 June 2023, San Diego, USA. Paper number AIAA 2023-4404. , 2023

Link: https://doi.org/10.2514/..

15

Large eddy simulations of isolated and installed jet noise ..:

Lindblad, Daniel ; Sherwin, Spencer J ; Cantwell, Chris...
Lindblad D, Sherwin SJ, Cantwell C, et al., (2023) Large eddy simulations of isolated and installed jet noise using the high-order discontinuous Galerkin method. In: AIAA SciTech Forum 2023, 23-27 January 2023, National Harbor, Maryland, USA. Paper number AIAA 2023-1546. , 2023

Link: https://doi.org/10.2514/..