Dear Students the Youtube Video has been uploaded for the following topics:Navier Stokes equation DerivationEnergy Equation DerivationDerivation - Momentum and Energy EquationBlasius solution for flow over a flat plate
Dear Students the Lecture Notes has been uploaded for the following topics:Introduction to basic Aerodynamics, Continuity equation , Momentum & energy equations , Aerodynamic forces and Moments , Viscous flow - Newton‘s law of viscosity- Viscous boundary layer , Methods to delay Flow Separation Flow over a flat plate, Blasius solution – Navier Stokes equation
Dear Students the Resource Link has been uploaded for the following topics:Derivation of Prandtl meyer equationOblique shockwaves
Dear Students the Youtube Video has been uploaded for the following topics:Derivation of Prandtl meyer equationNormal shockwavesMethod of Characteristics
Dear Students the Lecture Notes has been uploaded for the following topics:Airfoils Nomenclature and NACA series - Airfoil Characteristics , Vortex sheet - Kelvin Circulation theorem - Thin aerofoil theory and its applications , Introduction to Finite wing - Downwash and Induced Drag , Biot Savart law and Helmhotz‘s theorems - Horse shoe vortex , Prandtl‘s Classical Lifting line theory and its limitations , Prandtl equation and Rankine Hugoniot relation , Normal shock equations - Pitot static tube, corrections for subsonic and supersonic flows , Rayleigh and Fanno Flow – Flow past convex corners , Expansion hodograph - Reflection and interaction of shocks and expansion waves , Methods of Characteristics & Two-dimensional supersonic nozzle contours. , Small perturbation potential theory - Solutions for supersonic flows , Mach waves and Mach angles – Prandtl Glauert affine transformation relations for subsonic flows , Lift, drag pitching moment and center of pressure of supersonic profiles, linear theory - Linearised Supersonic flow theory - Linearised Velocity potential equation, CFD applications: Transonic Airfoil and wings – Supercritical airfoils , Lower and upper critical Mach numbers - Lift and drag divergence - shock induced separation , Wind tunnel types – Helium and gun tunnels , Characteristics of swept wings - Effects of thickness, camber and aspect ratio of wings , Shock tubes - Optical methods of flow visualization.
Dear Students the Question Bank has been uploaded for the following topics:Aerodynamics - I, Aerodynamics I, Aerodyanamics
