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Courses

  • Thermodynamics 1 (30112)
  • תקציר הקורס:

    Abstract:

    Fundamental concepts in thermodynamics, pure substance, heat, energy,

    work, first law of thermodynamic, heat engines in closed systems, the first law as a rate equation,

    enthalpy, the second law of thermodynamic and entropy, reversible process and Carnot heat engine,

    thermodynamic cycles in open systems, air cooling-heat pumps.
  • Heat Transfer (30120)
  • תקציר הקורס:

    Abstract:

    The course provides an elementary treatment of principles of Heat Transfer. Steady-State Conduction, Heat Exchangers, Steady State Conduction - Multiple dimension, Unsteady State Conduction, Forced Convection, Natural Convection, Radiation, Numerical method.
  • Fluid Mechanics And Measurements Laboratory (30161)
  • תקציר הקורס:

    Abstract:

    This course is designed to provide students with concepts in measuring systems, transducers and measuring devices, data logging systems, calibrations, thermal experiments, environmental conditions experiments.
  • Rocket Propulsion (30233)
  • תקציר הקורס:

    Abstract:

    General Introduction, Thrust Equation,

    Fundamentals, Performance of Rocket Engines, Equation of Motion,

     

    Staging, Analysis of Ideal Rocket and Nozzle Theory, Chemical Kinetics,

     

    Thermochemistry, Chemical Propellants, Solid Propellant Rockets,

     

    Liquid Propellant Rockets, Advanced Propulsion Systems.
  • Introduction To Aerodynamics (30328)
  • תקציר הקורס:

    Abstract:

    The objective of the course is to acquire general knowledge of the aerodynamics of aircrafts and the study of wing airfoils.

    This course is an introductory course emphasizing the historical background of aircraft development.

    The course will provide a review of the basics of flow while emphasizing aerodynamics.

    Development of Euler and Bernoulli equations. Flow around a cylinder in order to develop Kutta conditions.

    Thin wing (curvature, angle of attack). The effect of thickness. Finite wing (Vortex, Elliptical lift distribution), Prandtl's lift line, wind-tunnel corrections, concepts on flight at large angles of attack.