Structural Analysis of LRU box for a typical fighter aircraft

RS Vijaya Kumar , Manu j

vibration, Nastran, Shock loading, Arrestor loading, Fourier series, Normal modes

Design and analysis of 8 channel LRU box for typical fighter aircraft is conducted which is made of composite (CFRP) and Rohacell foam which is sandwiched construction, The LRU box is modeled in hyper mesh software of different thickness each thickness having different ply orientation. Material property is assigned. Shock loading analysis and arrestor landing analysis which is sinusoidal loading is done for different acceleration versus time profile and stress and displacement is found out for different time instant. Both simulated results and hand calculated results are calculated and is closely same.

Published Paper   E-Certificate

"Structural Analysis of LRU box for a typical fighter aircraft", IJSDR - International Journal of Scientific Development and Research (www.IJSDR.org), ISSN:2455-2631, Vol.1, Issue 9, page no.380 - 384, September-2016, Available :https://ijsdr.org/papers/IJSDR1609059.pdf

Volume 1 Issue 9, September-2016

Pages : 380 - 384

Paper Reg. ID: IJSDR_160825

Published Paper Id: IJSDR1609059

Downloads: 000347197

Research Area: Engineering

Country: bengaluru, karnataka, India

Published Paper PDF: https://ijsdr.org/papers/IJSDR1609059

Published Paper URL: https://ijsdr.org/viewpaperforall?paper=IJSDR1609059

ISSN: 2455-2631 | IMPACT FACTOR: 9.15 Calculated By Google Scholar | ESTD YEAR: 2016

An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 9.15 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator

Publisher: IJSDR(IJ Publication) Janvi Wave

This work is licensed under a Creative Commons Attribution 4.0 International License and The Open Definition