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NACA-TR-1204

Application of several methods for determining transfer functions and frequency response of aircraft from flight data

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1954

Abstract: In the process of analyzing the longitudinal frequency-response characteristics of aircraft, information on some of the methods of analysis has been obtained by the Langley Aeronautical Laboratory of the National Advisory Committee for Aeronautics. In the investigation of these methods, the practical applications and limitations were stressed. In general, the methods considered may be classed as: (1) analysis of sinusoidal response, (2) analysis of transient response as to harmonic content through determination of the Fourier integral by manual or machine methods, and (3) analysis of the transient through the use of least-squares solutions of the coefficients of an assumed equation for either the transient time response or frequency response (sometimes referred to as curve-fitting methods). (author)
URI: https://yse.yabesh.ir/std/handle/yse/39967
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    NACA-TR-1204

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:37:58Z
date available2017-09-04T15:37:58Z
date copyright01/01/1954
date issued1954
identifier otherOWRXYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/39967
description abstractIn the process of analyzing the longitudinal frequency-response characteristics of aircraft, information on some of the methods of analysis has been obtained by the Langley Aeronautical Laboratory of the National Advisory Committee for Aeronautics. In the investigation of these methods, the practical applications and limitations were stressed. In general, the methods considered may be classed as: (1) analysis of sinusoidal response, (2) analysis of transient response as to harmonic content through determination of the Fourier integral by manual or machine methods, and (3) analysis of the transient through the use of least-squares solutions of the coefficients of an assumed equation for either the transient time response or frequency response (sometimes referred to as curve-fitting methods). (author)
languageEnglish
titleNACA-TR-1204num
titleApplication of several methods for determining transfer functions and frequency response of aircraft from flight dataen
typestandard
page27
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1954
contenttypefulltext
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DSpace software copyright © 2017-2020  DuraSpace
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