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MECE 348 Aero Option
Home
Course Information
Course Weekly Syllabus
Aircraft Design - The Process
Aircraft Regulations
AIAA - Dec 2106 - Topics
Introductory Information
Design Parameters
Classification
Aircraft Structural Components
Aircraft Degree of Freedom
Weight Estimation
The Atmosphere
Altitude
Aircraft Speed
Aerodynamics-Lift
What is an Airfoil?
How Airfoil Produces Lift
Theoretical Calculation of Airfoil Lift
Airfoil Lift - Published
Finite Wings - Performance Loss
Finite Wings - Estimating Drag and Lift
Finite Wings - Theoretical Performance
Pressure Distribution - Airfoil and Wing
Aerodynamics -Drag
Drag - A Basic History
Boundary Layer
Skin Friction
Laminar and Turbulent Flow
Calculating Airplane Drag
Pressure Drag
Propulsion
Engine Types
Fuel Consumption
Propellor Performance
Piston Engine Analysis
Turbojet
Turboprop/Turboshaft
Turbofan
Ramjet
Rocket
Performance
Thrust Available
Helicopters
Two Planes
Flight in Vertical Plane
Steady Level Flight
Minimum Power and Speed
Climb Performance
Ceiling
Time to Climb
Range and Endurance - Jet
Range and Endurance - Propeller
Variation of Aero Coefficients
Takeoff Calculations
Landing Distance
Turing Flight
Effects of Mach Number
Density Changes
1 D Mass and Momentum and Energy
Stagnation and Static Values
Drag Effects of High Speed
Lift Effects at High Speed
Sound Barrier
Rocket Nozzles
The First M = 1 Car
Second Supersonic Car
Turbulence
Fluids BSME RIT
Turbulent Flow Decomposition
Turbulence Structure
RANS
k-e model
File Collection
Topics
Flying Taxis
Some Drag Coefficients
Space X Trajectory
Sustainability in Aerospace
What is it?
WIG Aircraft
Aerospace Designs (current)
MECE348 Syllabus 2155
Office Hours
References
Some Interesting Aerospace Links
MECE 348 Aero Option
The First M = 1 Car
Sonic Car
ThrustSSC was the first automobile (???) to break the sound barrier
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