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  Published Paper Details:

  Paper Title

NUMERICAL ANALYSIS OF AN AIRCRAFT PROTOTYPE MODEL BY USING NX NASTRAN

  Authors

  K Karthikeya

  Keywords

Aircraft, NX Nastran, FEM, Mode Shapes, Natural Frequencies.

  Abstract


Main aim of this paper is to determine modal analysis and numerical simulation to verify the structural characteristics of an aircraft. This paper details about natural frequencies and vibration mode shapes were obtained via measurement in NX Nastran. The frequency response function were identified and computed, FEM modal analysis was also implemented and its numerical results convincingly presented the mode shape and natural frequencies of aircraft is to be mentioned. Vibration response to different rotation speeds have been collected, managed and analyzed through the use of NX Nastran. Evident Phenomena have been discovered including the resonance on which most analysis is focused because of its potential use to generate larger amplitude vibration of specific frequency or to avoid such resonant frequencies from a wide spectrum of response.

  IJCRT's Publication Details

  Unique Identification Number - IJCRT2011207

  Paper ID - 200777

  Page Number(s) - 1705-1716

  Pubished in - Volume 8 | Issue 11 | November 2020

  DOI (Digital Object Identifier) -   

  Publisher Name - IJCRT | www.ijcrt.org | ISSN : 2320-2882

  E-ISSN Number - 2320-2882

  Cite this article

  K Karthikeya,   "NUMERICAL ANALYSIS OF AN AIRCRAFT PROTOTYPE MODEL BY USING NX NASTRAN", International Journal of Creative Research Thoughts (IJCRT), ISSN:2320-2882, Volume.8, Issue 11, pp.1705-1716, November 2020, Available at :http://www.ijcrt.org/papers/IJCRT2011207.pdf

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ISSN: 2320-2882
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Journal Starting Year (ESTD) : 2013
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ISSN and 7.97 Impact Factor Details


ISSN
ISSN
ISSN: 2320-2882
Impact Factor: 7.97 and ISSN APPROVED
Journal Starting Year (ESTD) : 2013
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