• Aircraft Wing Structure

    In aeronautics Wing are airfoils attached to each side of the fuselage, So the design of the wing depends on many facts like lift to weight ratio, rate of climb, size, weight and which aircraft it is used,

  • AirCraft Fuselage Structure

    Fuselage is a body of an aircraft to which the wings, tail and Landing Gear units are attached. Design and size of the fuselage varies according to the function to the aircraft. The word fuselage comes from a French word “fusele” means “splindle-shape”

  • Landing Gear

    Landing gear is an undercarriage part of the flight landing system. Aircraft landing gear has wheels equipped with shock absorbers on light planes and Hydraulic or pneumatic oleo struts on larger aircraft.

Showing posts with label Aerodynamics. Show all posts
Showing posts with label Aerodynamics. Show all posts

Monday, November 23, 2020

Types of flow in Aerodynamic

 

Different Types of flow in Aerodynamic

    Aerodynamics is a part fluid dynamics which deals with the laws of the flow of air or other gases.



Types of flow in Aerodynamic

  • Compressible Flow
  • Viscous Flow
  • Inviscid Flow
  • Steady Flow
  • Uniform Flow
  • Rotational Flow

Compressible Flow:  Compressible flow do undergo density changes, Gases are generally compressible.

Viscous Flow: The viscosity of a fluid is a measure of its resistance to gradual deformation by shearstress or tensile stress. Viscosity is due to the friction between neighboring particles in a fluid that are moving in different velocities.

Inviscid Flow: Is the flow of an ideal fluid that is assumed to have no viscosity.

Uniform Flow: It the flow velocity is the same magnitude and direction at every point.

Rotational Flow: If the angle between the two intersecting lines of the boundary of the fluid element changes while moving in the flow.