Courses
- Thermodynamics 2 (30113) תקציר הקורס:
- Heat Transfer (30120) תקציר הקורס:
- Fluid Mechanics and Measurements Laboratory (30161) תקציר הקורס:
- Rocket Propulsion (30233) תקציר הקורס:
- Introduction to Aerodynamics (30328) תקציר הקורס:
Abstract:
This course goal is to introduce students to thermodynamic
properties of pure substances and mixtures, and the interdependency of properties
of substances. The applicability of the First Law, Second Law, conservation of mass
and properties of substances in practical engineering systems, including gas mixtures
and power and refrigeration cycles will also be examined. In addition,
basic concepts of air conditioning will be studied while introducing
air-water vapor mixtures basic and the psychrometric diagram.
Fundamentals concepts of combustion reactions, enthalpy of formation
and heat of combustion will also be addressed.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.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.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.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.