Modelling and structural evaluation of honeycomb structure with frp composites

sk.mohammadh riyaz; v.seetha rami reddy

Modelling and structural evaluation of honeycomb structure with frp composites

Authors: sk.mohammadh riyaz, v.seetha rami reddy

Unique Paper ID: 154010
Volume: 8
Issue: 9
PageNo: 420-425

Keywords: CATIA modelling of the product static analysis Structural Analysis Thermal analysis strength.

Abstract:
Honeycomb structures are natural or man-made structures that have the geometry of a honeycomb to allow the minimization of the amount of used material to reach minimal weight and minimal material cost. Types of honeycomb structures are depending upon the geometrical shape. There are different types of honeycomb core structures like square, hexagonal, pentagonal, tetrahedral, pyramidal etc. In this project we are comparing the structural analysis for square and hexagonal honeycomb structures and thermal analysis of square and hexagonal honeycomb structures. Structural analysis is the determination of the effects of loads on physical structure. To perform an accurate analysis an engineer must determine such information as structural loads, geometry, support conditions, and materials properties. The results of such an analysis typically include deformation, stresses and displacements. This information is then compared to criteria that indicate the conditions of failure. Thermal analysis calculates the temperature distribution and related thermal quantities in the system or component. Typical thermal quantities of interest are: The temperature distributions:(a) The time to reach steady state, (b) The steady state temperature distribution (using a transient analysis), (c) The temperature distribution after 50 seconds; The amount of heat lost or gained; Thermal gradients; Thermal fluxes.

Download article

email to a friend

Cite This Article

ISSN: 2349-6002
Volume: 8
Issue: 9
PageNo: 420-425

Modelling and structural evaluation of honeycomb structure with frp composites

Available:https://ijirt.org/Article?manuscript=154010

18 Jun, 2022

DESIGN AND ANALYSIS OF GAS TURBINE COMBUSTION CHAMBER

18 Feb, 2022

DESIGN AND ANALYSIS OF SIX STROKE CYLINDER BLOCK

03 Mar, 2019

STUDY ON DESIGN AND PERFORMANCE COMPARISON OF RC BUILDINGS DESIGNED FOR VARIOUS INDIAN SEISMIC ZONES

18 Jun, 2018

SEISMIC ANALYSIS AND DESIGN OF VERTICALLY IRREGULAR RC BUILDING FRAMES

18 Jun, 2018

EXPERIMETAL AND ANALYTICAL STUDY ON TORSIONAL BEHAVIOR OF RC FLANGED BEAMS STRENGTHENED WITH GLASS FRP

18 Jun, 2022

DESIGN AND ANALYSIS OF AIRCARFT TRUSS USING ANYSIS

18 Jun, 2022

ULTRA HIGH TEMPERATURE CERAMICS FOR HYPERSONIC VEHICLE APPLICATIONS (ROCKET NOZZLE)

18 Jun, 2022

Design and optimization of body mount bracket of SUV car

18 Jun, 2022

DESIGN AND ANALYSIS OF AIRCRAFT COOLING FAN

18 Jun, 2022

DESIGN AND ANALYSIS OF FIN BLADES OF CARGO AEROPLANE

18 Jun, 2022

DESIGN AND ANALYSIS OF GAS TURBINE COMBUSTION CHAMBER

18 Feb, 2022

DESIGN AND ANALYSIS OF SIX STROKE CYLINDER BLOCK

03 Mar, 2019

STUDY ON DESIGN AND PERFORMANCE COMPARISON OF RC BUILDINGS DESIGNED FOR VARIOUS INDIAN SEISMIC ZONES

18 Jun, 2018

SEISMIC ANALYSIS AND DESIGN OF VERTICALLY IRREGULAR RC BUILDING FRAMES

18 Jun, 2018

EXPERIMETAL AND ANALYTICAL STUDY ON TORSIONAL BEHAVIOR OF RC FLANGED BEAMS STRENGTHENED WITH GLASS FRP

18 Jun, 2022

DESIGN AND ANALYSIS OF AIRCARFT TRUSS USING ANYSIS

18 Jun, 2022

ULTRA HIGH TEMPERATURE CERAMICS FOR HYPERSONIC VEHICLE APPLICATIONS (ROCKET NOZZLE)

18 Jun, 2022

Design and optimization of body mount bracket of SUV car

18 Jun, 2022

DESIGN AND ANALYSIS OF AIRCRAFT COOLING FAN

18 Jun, 2022

DESIGN AND ANALYSIS OF FIN BLADES OF CARGO AEROPLANE

Impact Factor
8.01 (Year 2024)

UGC Approved
Journal no 47859

Join Our IPN

IJIRT Partner Network

Submit your research paper and those of your network (friends, colleagues, or peers) through your IPN account, and receive 800 INR for each paper that gets published.

Join Now

Latest Publication

Recent Conferences

NCSEM 2024

National Conference on Sustainable Engineering and Management - 2024 Last Date: 15th March 2024

Submit inquiry