Lettering; orthographic projections; sketching and drawing; pictorial drawing; dimensioning; to lerancing and geometrical tolerancing; section; working drawing; mechanical parts drawing; introduction to CAD.

Overview ofaerospaceengineering withafocusonusing group projects toenhance critical thinking and problem solving applied to aerospace engineering related problems; group projects will facilitate creativity in solving complex problems, as well as communication and collaboration between students; introductory aerodynamics including lift, drag and the standard atmosphere; aircraft performance, stability, and control; propulsion; structures; rocket and spacecraft trajectories and orbits; introduction to unmanned aerial vehicles and applications of artificial intelligence in autonomous flight.

Introduction to aerospace design methodology and system engineering with a focus on systematic and critical thinking skill; Group design projects based on real world p roblems to enhance creat ivity, team communication, collaboration; fundamental to aircraft systems; requirements discovery and analysis process; introduction to elements of aerodynamic, airfoi ls, and wings, aspect of vehicle conceptual design; configuration s section; aircraft initial sizing; introduction to novel aerospace design concept such as unmanned aerial v ehicles, urban airmobility vehicle, and integration of artificial intelligence in modern aerospace design.

Engineering solutions to the 21st century problems; fundamental skill and tools in engineering; design thinking process; problem solving skill; introduction to data science, product design, ecological and pollution management and disaster mitigation; innovation business idea development, feasibility analysis, project planning, business idea presentation.

Use of Python, R, or similar tool to understand computing for scientific purposes. Includes data management, numerical computations, symbolic computing, data visualization, data analysis, parallel computing, and high-performance computing. Use of reallife case studies in scientific computing.

Computer programming in Engineering; reviews of computer programming concepts; hands on experience on computer programming using contemporary engineering tools

Analysis of force systems and their equilibrium as applied to engineering systems; stresses and strains; mechanical properties of materials; Hooke’s law, elastic modulus, stress in beam, shear force, bending moment diagram, torsion, buckling of columns, Mohr’s circle.

Basic concepts; thermodynamic state and process; properties of pure substances and ideal gases; energy; the first law of thermodynamics and the first law analysis for isolated, closed, and open systems; entropy; the second law of thermodynamics and the second law analysis for isolated, closed, and opens systems; gas power cycles; Carnot, Otto, and Brayton cycles; refrigeration cycle; introduction to gas mixtures; introduction to combustion.

Basic concepts in physics: physical quantity and physical quantity relations, dimensions of physical quantity and the principle of dimensional homogeneity, dimensionless variables; basic concepts in fluid mechanics: continuum assumption, methods of description: Lagrangian and Eulerian descriptions, field quantity and classification of flow fields; geometric and kinematics of fluid motion: path lines, streamlines, and streak lines; forces and stressed in fluids: pressure and pressure force, shear stress and shear force: convection flux and Reynold’s transport theorem; physical laws of finite control volume: conservations of mass, linear momentum, and energy; conservation of angular momentum with application to turbomachines; physical laws of infinite control volume: conservation of mass and linear momentum, introduction to Navier-Stokes and Euler’s equations; Bernoulli’s equation from momentum and conservation of mechanical energy viewpoints; introduction to vorticity and vortex; dimensional analysis: Buckingham’s PI theorem, similarity, and model testing; internal viscous flows, energy consideration in pipe flows and piping system; external flows, boundary layer, and aerodynamic force and moment; applications: turbomachines, model testing, piping and pumping system, aerodynamic force and moment.

Kinematics of three-dimensional curvilinear motion of a particle; kinetics of a particle: force and acceleration, work and energy, impulse and momentum; kinematics of planar motion of a rigid body: absolute and relative motion analysis; kinetics of planar motion of a rigid body: force and acceleration, work and energy, impulse and momentum; introduction to kinematics and kinetics of three-dimensional motion of a rigid body.

Important engineering materials: metals, plastics, asphalt, wood and concrete; macroscopic and microscopic structure which are correlating with properties of the engineering materials; production process of products from engineering materials

CONDITION: PRER 2183222
Atmosphere and properties of air; airfoil geometry; aerodynamic forces; stream function; vorticity and circulation; elementary flows; incompressible flow over aerofoils; irrotational flow; lifting flow; the Kutta Joukowski theorem; Kutta condition; Kelvin’s circulation theorem and starting vortex; thin aerofoil theory; flapped aerofoil; thick cambered aerofoil; maximum lift coefficient a nd stall; high lift devices; incompressible flow over finite wings; Prandtl’s lifting line theory; elliptical and general lift distribution; fundamental of viscous flow; conservation of mass and continuity equation; conservation of momentum and momentum equation; boundary layers; flow instabilities; turbulence.

CONDITION: PRER 2183221 and 2145311
Fundamental of compressible flow, acoustic waves, normal and oblique shock waves, expansion waves, Prandtl-Meyer flow, convergent-divergent nozzle, flow with friction and heat transfer, unsteady wave motion, perturbation theory, linearized flow and theory of characteristics.

CONDITION: PRER 2183221 and 2183222
Introduction to propulsion, air-breathing and non-air-breathing engines; brief review of the thermodynamics and compressible flow; basic thrust equation of aircraft gas turbine and jet engines; Brayton cycle, axial flow turbomachines, momentum theory and blade element theory; gas turbine component performance, inlet, compressor, turbine and nozzle; cycle analysis of gas turbine engines, rocket, ramjet, turbojet, turbofan and turboprop covering introduction to preliminary propulsion design

Overview of aircraft structural external loads analysis including criteria, design, analysis, fatigue, certification, validation, and testing. Covers FAR 23 and FAR 25 airplane loads requirements. Includes introduction to the use of finite element package in structural analysis. Course will provide students with an understanding of fuselage/wing design and analysis including frames and ribs. Also provides an introduction to structural dynamics including aeroelasticity.

Principles of jet and propeller aircraft performance; equations of motions; cruise flight, climb and descent; turning flight; takeoff and landing performance; range and endurance; payload-range diagram; maneuvering V-n diagram.

Basic avionic system, air data systems, flight instruments, terrestrial en-route – radio navigation systems, terrestrial landing aids, satellite navigation system, radar systems, indicators and displays, airborne radio communications, autopilot and flight-management system, avionics systems integration

Equilibrium and stability; functions of aircraft controls; static stability and trim; stability derivatives for longitudinal motions; stick-fixed, stick-free and control stick forces; wing and tail contributions; maneuver stability; roll stability and roll control; yaw stability and yaw control; dynamic behavior of aircraft and equations of motion; phugoid and short period oscillation; Dutch roll; spiral mode and roll subsidence; dihedral effect and weathercock stability.

Concepts in experimentation; introduction to systematic design of an experiment using data reduction diagram (DRD): setting up objectives of an experiment, constructing the set of data reduction diagrams (DRDs) of the experiment according to the objectives; measurement and instrument; uncertainty analysis; basic experiments and laboratories in thermodynamics; fluid mechanics and aerodynamics; dynamics; solid mechanics

CONDITION: PRE-REQUISITE 2145361
Experiments and laboratories in aerodynamics, structure, propulsion, performance, dynamics and control

CONDITION: PRE-REQUISITE 2145362
Concepts in experimentation and design of an experiment; setting up specifications and objectives of an experiment; systematic design of an experiment according to the specifications and objectives using different kinds of tools; outlining the process of extracting experimental results and conclusions from the designed experiment; outlining data collection and data analysis schemes outlining experimental project phases, tasks, and schedule; design documentation and review by oral and written presentation; practices in the design of an experiment in the project-based setting; introduction to modern instrumentation and data acquisition through demonstration 1) Identify the motivation for the project with specific and relevant applications, background knowledge, and underlying ideas, of the project. 2) Formulate clear problem/objective and scope of the project. If it is a design project, engineering specifications of the design must be provided. 3) Propose, in principle, the approach you will be using in solving the problem, and/or the conceptual design, and/or the principle of your experiment or simulation. 4) Some preliminary solution, and/or design, and/or experimental or simulation results, demonstrating the effectiveness of your proposed approach in (3), or the ineffectiveness of your approach in (3) and the potential remedies/alternatives for the approach, must be provided. Group or individual project. The students must propose the project in writing and oral presentation. Remark: Engineering specifications are derived from necessities, needs, and preferences of the use, constraints and conditions, as well as safety, environmental, manufacturability, and economic considerations

Fundamentals of aircraft design process including wing design, tail design, and undercarriage arrangement. Also covers initial take-off mass estimation, detailed mass calculation, and mission fuel requirement. Incorporates principles from prior aerospace engineering courses including center of gravity calculation, basic aerodynamics estimation, static stability and control analysis, propulsion consideration and analysis, performance analysis, aircraft cost prediction, preliminary and detailed design concepts, quality control of aircraft design.

Identify the aerospace engineering project of interest and propose the project to be conducted in 2145499 Aerospace Engineering Project course. This necessarily constitutes at least the followings. 1) Identify the motivation for the project with specific and relevant applications, background knowledge, and underlying ideas, of the project. 2) Formulate clear problem/objective and scope of the project. If it is a design project, engineering specifications of the design must be provided. 3) Propose, in principle, the approach you will be using in solving the problem, and/or the conceptual design, and/or the principle of your experiment or simulation. 4) Some preliminary solution, and/or design, and/or experimental or simulation results, demonstrating the effectiveness of your proposed approach in (3), or the ineffectiveness of your approach in (3) and the potential remedies/alternatives for the approach, must be provided. Group or individual project. The students must propose the project in writing and oral presentation. Remark: Engineering specifications are derived from necessities, needs, and preferences of the use, constraints and conditions, as well as safety, environmental, manufacturability, and economic considerations

CONDITION: PRE-REQUISITE 2145479
Completion of the aerospace engineering project. The students must demonstrate systematic and sound approach in conducting the project, from beginning to end. Some degree of the evaluation of the project must be provided. Report and present the project professionally

Discussion on the topics of aerospace engineering

Discussion on the topics of aerospace engineering

Discussion on the topics of aerospace engineering

Engineering practice in related areas under supervision of experienced engineers in private sectors or government agencies