Das Buch basiert auf der Untersuchung der Leistung verschiedener Tragflächenformen bei unterschiedlichen Anstellwinkeln durch die Durchführung numerischer Untersuchungen. Die Leistung der Tragflächenformen wurde anhand des Kriteriums der Auftriebskrafterzeugung bewertet, da die Tragflächen so gestaltet sind, dass sie ein Maximum an Auftrieb erzeugen. Verschiedene Diagramme wie Geschwindigkeitskonturen, Auftriebs- und Widerstandskoeffizient in Abhängigkeit von den verschiedenen Anstellwinkeln wurden ebenfalls aufgezeichnet, um die Leistung der verschiedenen Tragflächenformen zu bewerten.
Das Buch basiert auf der Untersuchung der Leistung verschiedener Tragflächenformen bei unterschiedlichen Anstellwinkeln durch die Durchführung numer...
The book is founded on investigating the performance of different aerofoil shapes at varying angles of attack by conducting numerical investigation. The performance of the aerofoil shapes has been evaluated on the basis of the criterion of lift force generation as the aerofoils are designed in such a way that they generate maximum amount of lift. Different plots such as velocity contours and coefficient of lift and coefficient of drag versus different angles of attack have also been plotted for assessing the performance of different aerofoil shapes.
The book is founded on investigating the performance of different aerofoil shapes at varying angles of attack by conducting numerical investigation. T...
Le livre est fondé sur l'étude de la performance de différentes formes d'aérofreins à des angles d'attaque variables en effectuant des recherches numériques. Les performances des profils aérodynamiques ont été évaluées sur la base du critère de génération de force de portance, les profils aérodynamiques étant conçus de manière à générer une portance maximale. Différents graphiques tels que les contours de vitesse, le coefficient de portance et le coefficient de traînée en fonction des différents angles d'attaque ont également été tracés pour évaluer les...
Le livre est fondé sur l'étude de la performance de différentes formes d'aérofreins à des angles d'attaque variables en effectuant des recherches...
The work presented in the book deals with design analysis and material selection for the retractable shield by considering the stress-induced and deformation under controlled conditions of the working environment. Weight and mobility of the shield are also considered as prime factors while carrying out the analysis. A comparison among different shield materials is carried out and the selection of suitable material is based on the basis of numerical analysis.
The work presented in the book deals with design analysis and material selection for the retractable shield by considering the stress-induced and defo...
The book entitled, "STUDY AND ANALYSIS OF FERROFLUID BASED PASSIVE COOLING DEVICE" is founded on investigating the performance of ferrofluid based cooling device using numerical simulation. The effect of orientation of permanent magnet with respect to heat source and number of fins on the performance of the system is evaluated. COMSOL Multiphysics software was used to carry out the simulation work with magnet placed in different orientations ranging from zero to 135 degree and with number of fins varying from 26-42. The results have been presented by drawing plots such as Nusselt number,...
The book entitled, "STUDY AND ANALYSIS OF FERROFLUID BASED PASSIVE COOLING DEVICE" is founded on investigating the performance of ferrofluid based coo...