4/5/2023 0 Comments Double wedge airfoilResults obtained from manual calculations and fluent analysis are cross checked.ĪB - Aeronautical studies are being focused more towards supersonic flights and methods to attain a better and safer flight with highest possible performance. MATLAB is used to form a code for obtaining shock angle with Mach number and wedge angle at the given parameters. Manual calculations for oblique shock properties are calculated with the help of Microsoft excel. Analysis is carried out using fluent at standard conditions with specific heat ratio taken as 1.4. Double wedge airfoil is analysed at different Angles of attack (AOA) based on the wedge angle. Available Computational tools are utilized for analysis. Physical parameters considered for the Double wedge case with wedge angle (ranging from 5 degree to 15 degree. Mach number range taken is for transonic and supersonic. The present work is based on the effects of change in physical parameter for the Double wedge airfoil. Airfoil shapes differ based on the applications, hence the airfoil shapes considered for supersonic speeds are different from the ones considered for Subsonic. Aerodynamic analysis is part of the whole procedure, which includes focusing on airfoil shapes which will permit sustained flight of aircraft at these speeds. N2 - Aeronautical studies are being focused more towards supersonic flights and methods to attain a better and safer flight with highest possible performance. T1 - Aerodynamic Analysis over Double Wedge Airfoil Results obtained from manual calculations and fluent analysis are cross checked.", Results obtained from manual calculations and fluent analysis are cross checked.Ībstract = "Aeronautical studies are being focused more towards supersonic flights and methods to attain a better and safer flight with highest possible performance. Aeronautical studies are being focused more towards supersonic flights and methods to attain a better and safer flight with highest possible performance.
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