NEW YORK
METROPOLITAN
UNIVERSITY

Graduate Diploma in Engineering in Aerospace Engineering

  • Eligibility Criteria

    Bachelor's degree, or equiv. International Education

  • Credit Hours

    30

  • Courses Offered

    5

  • Course Duration

    6 Months (Self-Paced) Program

  • Estimated Fee

    $6,450

Courses Offered

A graduate diploma by NYMU allows you to cement your growth as a human being as it offers opportunity to engage in discovering endless firms and reputable corporations so you can secure your ideal life.

Introduction To Propulsion (AEE-152)

TOPICS COVERED IN THIS COURSE
  In Section 1 of this course you will cover these topics:
     The Jet Propulsion Principle
     Mechanics And Thermodynamics Of Fluid Flow
     Steady One-Dimensional Flow Of A Perfect Gas
  In Section 2 of this course you will cover these topics:
     Boundary Layer Mechanics And Heat Transfer
     Thermodynamics Of Aircraft Jet Engines  
     Aerodynamics Of Inlets, Combustors, And Nozzles
  In Section 3 of this course you will cover these topics:
     Axial Compressors
     Axial Turbines
     The Centrifugal Compressor
  In Section 4 of this course you will cover these topics:
     Performance Of Rocket Vehicles
     Chemical Rocket Thrust Chambers
  In Section 5 of this course you will cover these topics:
     Chemical Rocket Propellants: Combustion And Expansion
     Turbomachinery For Liquid-Propellant Rockets
     Electrical Rocket Propulsion

Gas Dynamics (AEE-273)

TOPICS COVERED IN THIS COURSE
  In Section 1 of this course you will cover these topics:
     Basic Equations Of Compressible Flow
     Wave Propagation In Compressible Media
     Isentropic Flow Of A Perfect Gas
  In Section 2 of this course you will cover these topics:
     Stationary Normal Shock Waves
     Moving Normal Shock Waves
     Oblique Shock Waves
  In Section 3 of this course you will cover these topics:
     Pr And Tl Meyer Flow
     Applications Involving Shocks And Expansion Fans
     Flow With Friction
  In Section 4 of this course you will cover these topics:
     Heat Addition
     Equations Of Motion For Multidimensional Flow
     Linearized Flow
  In Section 5 of this course you will cover these topics:
     Methods Of Characteristics
     Computational Gas Dynamics
     Differential Analysis Of Fluid Flow

Introduction To Aerodynamics (AEE-349)

TOPICS COVERED IN THIS COURSE
  In Section 1 of this course you will cover these topics:
     Fluid Properties
     Fundamentals Of Fluid Mechanics
     Dynamics Of An Incompressible, Inviscid Flow Field
  In Section 2 of this course you will cover these topics:
     Viscous Boundary Layers
     Characteristic Parameters For Airfoil And Wing Aerodynamics
     Incompressible Flows Around Airfoils Of Infinite Span
  In Section 3 of this course you will cover these topics:
     Incompressible Flows About Wings Of Finite Span
     Dynamics Of A Compressible Flow Field
     Compressible, Subsonic Flows And Transonic Flows
  In Section 4 of this course you will cover these topics:
     Two-Dimensional Supersonic Flows Around Thin Airfoil
     Supersonic Flows Over Wings And Airplane Configurations
     Hypersonic Flows
  In Section 5 of this course you will cover these topics:
     Aerodynamic Design Considerations
     Tools For Defining The Aerodynamic Environment

Aircraft Electric Systems (AEE-625)

TOPICS COVERED IN THIS COURSE
  In Section 1 of this course you will cover these topics:
     Direct Current Power Supplies
     Alternating Current Power Supplies
     Power Conversion Equipment
  In Section 2 of this course you will cover these topics:
     External And Auxiliary Power Supplies
     Power Distribution
  In Section 3 of this course you will cover these topics:
     Circuit Controlling Devices
     Circuit Protection Devices And Systems
  In Section 4 of this course you will cover these topics:
     Measuring Instruments And Warning Indication Systems
     Power Utilization Motors
  In Section 5 of this course you will cover these topics:
     Power Utilization Systems
     Electrical Diagrams And Identification Schemes

Fundamentals Of Flight (AEE-635)

TOPICS COVERED IN THIS COURSE
  In Section 1 of this course you will cover these topics:
     Conversion Factors Between Si Units And English Units
     Nomenclature
     A Brief History Of Aeronautics
     The Anatomy Of The Airplane
     The Nature Of Aerodynamic Forces: Dimensional Analysis
  In Section 2 of this course you will cover these topics:
     Theory And Experiment Wind Tunnels
     The Atmosphere
     Incompressible One-Dimensional Flow
     One-Dimensional Flow In A Compressible Fluid
     Two-Dimensional Flow: Lift And Drag
  In Section 3 of this course you will cover these topics:
     The Finite Wing
     Effects Of Viscosity
     Determination Of Total Incompressible Drag
     Compressibility Drag
  In Section 4 of this course you will cover these topics:
     Airfoils And Wings
     High-Lift Systems
     Aerodynamic Performance
     Stability And Control
  In Section 5 of this course you will cover these topics:
     Propulsion
     Structures
     Hypersonic Flow
     Rocket Trajectories And Orbits

Why Choose New York Metropolitan University

New York Metropolitan University is the name of excellence, and we emphasize fully working on the future of our students just so they can reach their true potential. Our unparalleled campus experience allows students of all races and religions to excel in their abilities. Here, you are not just growing in your educational career; you can also focus on and enhance your extracurricular activities. We are passionate about providing you with the best overall experience before you enter your professional career path. However, the real career paths of students begin with us.