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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
Turing Flight
Steady level turn in a horizontal plane (Banking Flight)
Pull up - Steady turn in vertical plane
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