Defects are often arises on the inner surface of aircraft structures, but most of conventional techniques can determine only the damages and cannot determine the degree of damage. Digital Image Processing and Wavelet Transform are used in this project. Characteristics parameters such as the length of the crack can be exactly detected to measure the faults of...
Showing posts with label Aeronautical Engineering. Show all posts
Showing posts with label Aeronautical Engineering. Show all posts
Wednesday, 21 July 2021
Tuesday, 20 July 2021
Computational Investigation on the Effect of Fences on Aerodynamic Characteristics of an Aircraft Wing
Team IJTSRD
July 20, 2021
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A computational study, to improve the stall characteristics of wing at high angles of attack, with and without fence configuration is done here. Wing fences, also known as boundary layer fences and potential fences are fixed aerodynamic devices attached to aircraft in the exactly middle of the span and two fences are fixed in the exactly middle of the wing span...
Saturday, 18 April 2020
Comparative Study on Effective Turbulence Model for NACA0012 Airfoil using Spalart – Allmaras as a Benchmark
Team IJTSRD
April 18, 2020
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The present work is dedicated to conduct a comparative study on identifying the effective turbulence model in terms of flow outlet velocity, error percentage, number of iterations and time coefficient using NACA0012 airfoil by considering Spalart – Allmaras as a reference model. The current study considers 12 different turbulence models including Spalart...
Monday, 6 January 2020
The Impact of Temperature and Relative Humidity Elevation on Mental Health of In Patient Admitted Into Jos Teaching Hospital Jos, Plateau State, Nigeria
Team IJTSRD
January 06, 2020
0
The paper examined the impact of temperature and relative humidity escalation on mental health of in patient admitted into Jos Teaching Hospital JUTH Jos, Plateau State, Nigeria. The main independent variables of interest were temperature and relative humidity we also employed two derived parameters heat index and overlapping effect in our analysis in which...
