scholarly journals Model-scale jet noise analysis with a single-point, frequency-domain nonlinearity indicator

2018 ◽  
Vol 143 (6) ◽  
pp. 3479-3492 ◽  
Author(s):  
Kyle G. Miller ◽  
Kent L. Gee
2017 ◽  
Vol 2017 ◽  
pp. 1-13
Author(s):  
Can-bin Yin ◽  
Da Ran

Novel frequency domain extracted method (FDEM) to obtain high range resolution profile (HRRP) for frequency stepped synthetic aperture radar (SAR) is proposed in this paper, and the mathematical principle and formulas of this new HRRP obtaining idea combined with classical fast Fourier transform (FFT), chirp z transform (CZT), and single point Fourier transform (SPFT) are deduced, analyzed, and compared in detail. Based on the HRRP data, precision imaging processing is completed using a data block partition based fast factorized back projection algorithm. Imaging validations are executed and all results proved that the FDEM has a great capability of antijamming. It is more effective than conventional time domain IFFT method (TDM) and shows a great promise in frequency stepped radar imaging and applications.


2020 ◽  
Vol 24 (11-12) ◽  
pp. 3059-3071 ◽  
Author(s):  
S. Martemianov ◽  
A. Thomas ◽  
N. Adiutantov ◽  
E. Denisov ◽  
Yu Evdokimov ◽  
...  

2005 ◽  
Vol 4 (3) ◽  
pp. 289-323 ◽  
Author(s):  
K.M. Khritov ◽  
V.Ye. Kozlov ◽  
S.Yu. Krasheninnikov ◽  
A.B. Lebedev ◽  
D.A. Lyubimov ◽  
...  

Several experimental, computational and theoretical results devoted to turbulence jet noise are described. All these results were obtained at CIAM in collaboration with the Boeing Company. The selected topics are combined and described from a single point of view. In spite of the many publications in the classical literature devoted to jet noise, many jet noise problems are not completely solved, and most current jet noise prediction methods are still highly empirical and rely heavily on an existing experimental data base. At the same time, many of the available experimental results are not fully reliable and some are even contradictory. The goal of this paper is, therefore, to explore and discuss some of the possibilities and limitations of classical aeroacoustics methods.


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