Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781723906183
Category :
Languages : en
Pages : 66
Book Description
A method to separate main rotor and tail rotor noise from a helicopter in flight is explored. Being the sum of two periodic signals of disproportionate, or incommensurate frequencies, helicopter noise is neither periodic nor stationary, but possibly harmonizable. The single Fourier transform divides signal energy into frequency bins of equal size. Incommensurate frequencies are therefore not adequately represented by any one chosen data block size. A two-dimensional Fourier analysis method is used to show helicopter noise as harmonizable. The two-dimensional spectral analysis method is first applied to simulated signals. This initial analysis gives an idea of the characteristics of the two-dimensional autocorrelations and spectra. Data from a helicopter flight test is analyzed in two dimensions. The test aircraft are a Boeing MD902 Explorer (no tail rotor) and a Sikorsky S-76 (4-bladed tail rotor). The results show that the main rotor and tail rotor signals can indeed be separated in the two-dimensional Fourier transform spectrum. The separation occurs along the diagonals associated with the frequencies of interest. These diagonals are individual spectra containing only information related to one particular frequency.Santa Maria, Odilyn L.Langley Research CenterFOURIER TRANSFORMATION; AIRCRAFT NOISE; FOURIER ANALYSIS; AERODYNAMIC NOISE; AEROACOUSTICS; HELICOPTERS; SPECTRUM ANALYSIS; FLIGHT TESTS; TAIL ROTORS
Two-Dimensional Fourier Transform Applied to Helicopter Flyover Noise
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781723906183
Category :
Languages : en
Pages : 66
Book Description
A method to separate main rotor and tail rotor noise from a helicopter in flight is explored. Being the sum of two periodic signals of disproportionate, or incommensurate frequencies, helicopter noise is neither periodic nor stationary, but possibly harmonizable. The single Fourier transform divides signal energy into frequency bins of equal size. Incommensurate frequencies are therefore not adequately represented by any one chosen data block size. A two-dimensional Fourier analysis method is used to show helicopter noise as harmonizable. The two-dimensional spectral analysis method is first applied to simulated signals. This initial analysis gives an idea of the characteristics of the two-dimensional autocorrelations and spectra. Data from a helicopter flight test is analyzed in two dimensions. The test aircraft are a Boeing MD902 Explorer (no tail rotor) and a Sikorsky S-76 (4-bladed tail rotor). The results show that the main rotor and tail rotor signals can indeed be separated in the two-dimensional Fourier transform spectrum. The separation occurs along the diagonals associated with the frequencies of interest. These diagonals are individual spectra containing only information related to one particular frequency.Santa Maria, Odilyn L.Langley Research CenterFOURIER TRANSFORMATION; AIRCRAFT NOISE; FOURIER ANALYSIS; AERODYNAMIC NOISE; AEROACOUSTICS; HELICOPTERS; SPECTRUM ANALYSIS; FLIGHT TESTS; TAIL ROTORS
Publisher: Independently Published
ISBN: 9781723906183
Category :
Languages : en
Pages : 66
Book Description
A method to separate main rotor and tail rotor noise from a helicopter in flight is explored. Being the sum of two periodic signals of disproportionate, or incommensurate frequencies, helicopter noise is neither periodic nor stationary, but possibly harmonizable. The single Fourier transform divides signal energy into frequency bins of equal size. Incommensurate frequencies are therefore not adequately represented by any one chosen data block size. A two-dimensional Fourier analysis method is used to show helicopter noise as harmonizable. The two-dimensional spectral analysis method is first applied to simulated signals. This initial analysis gives an idea of the characteristics of the two-dimensional autocorrelations and spectra. Data from a helicopter flight test is analyzed in two dimensions. The test aircraft are a Boeing MD902 Explorer (no tail rotor) and a Sikorsky S-76 (4-bladed tail rotor). The results show that the main rotor and tail rotor signals can indeed be separated in the two-dimensional Fourier transform spectrum. The separation occurs along the diagonals associated with the frequencies of interest. These diagonals are individual spectra containing only information related to one particular frequency.Santa Maria, Odilyn L.Langley Research CenterFOURIER TRANSFORMATION; AIRCRAFT NOISE; FOURIER ANALYSIS; AERODYNAMIC NOISE; AEROACOUSTICS; HELICOPTERS; SPECTRUM ANALYSIS; FLIGHT TESTS; TAIL ROTORS
Two-Dimensional Fourier Transform Applied to Helicopter Flyover Noise
Author: Odilyn L. Santa Maria
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 70
Book Description
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 70
Book Description
NASA Langley Scientific and Technical Information Output: 1999
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 182
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 182
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 776
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 776
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 304
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 304
Book Description
International Aerospace Abstracts
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1042
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1042
Book Description
Vertiflite
Author:
Publisher:
ISBN:
Category : Helicopter
Languages : en
Pages : 1180
Book Description
Publisher:
ISBN:
Category : Helicopter
Languages : en
Pages : 1180
Book Description
Verti-flite
Author:
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 594
Book Description
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 594
Book Description
Master's Theses Directories
Author:
Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 492
Book Description
"Education, arts and social sciences, natural and technical sciences in the United States and Canada".
Publisher:
ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 492
Book Description
"Education, arts and social sciences, natural and technical sciences in the United States and Canada".
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Book Description