Department Home

AA 461

Course Home

Course Outline

Homework & Solutions

Reference Material

     10/1    Compressor Terminology  Euler Turbine Equation Development-1  Euler Turbine Equation Development-2 

Forces on Compressor Blades 

Turbine Velocity Diagram-1  Turbine Velocity Diagram-2  Turbine Velocity Diagram-3  Turbine Velocity diagram-4 

Sketch of Fighter Jet Engine Location

 

HP Compressor Rotor

HP Compressor Stator

Shocks_Over_Compressor Blades

Compressor Definition Sketch

Turbofan Schematic Diagram

“Triple Spool” Engine Configuration

 

     10/22   Methane/Air Adiabatic Flame Temperature Calculation Spreadsheet

GasEq Setup Screenshot

GasEq Methane/Air example

GasEq Methane/Air Combustion with “extended” chemistry

GasEq Methane/Air Combustion with “major species” only

H2O Equilibrium Calculation using GasEq

H2O Equilibrium  Plots

Can Combustor Configuration

Can Combustor Showing Combustion

Annular Combustor

Twin Swirler Annular Combustor Face

 

     10/27   Hydrogen/Oxygen Reactions

RQL Combustor Concept

Two Staged Combustor Concepts

Combustor with Exhaust Gas Recirculation

Trends in NO, CO, and Soot Formation

 

     10/30   Turbine: “Nozzle” and “Bucket” Configuration Sketch

Turbine Velocity Diagram

Impulse vs. Reaction Turbines 1

Impulse vs. Reaction Turbines 2

Shock in Turbine

Turbine Cooling Schematic

Cooled Turbine Blade Cutaway 1

Cooled Turbine Blade Cutaway 2f

F100 Turbine Blade 1

F100 Turbine Blade 2

 

Review Notes for Mid-Term

 

     11/26   Afterburner\afterburner.JPG

 

     11/26   Commercial vs. Military Inlets

F16_Inlet

Another F16_ Inlet

Typical Military Inlet Installation

Mirage 2000 Inlet

SR-71 Inlet.JPG

 

     11/26   2D Nozzle.JPG

Another 2D Nozzle

F404 CD Nozzle

F16 CD Nozzle

“Hot Stream” (Clamshell) Thrust Reverser

“Cold Stream” Thrust Reverser

Corrugated (“Daisy”) Mixer Nozzle

External vs. Internal Nozzle Stream Mixing

Gas Turbine Nozzle Noise Breakdown

 

     11/26   Delta 4 Rocket Launch

Space Shuttle Launch

Effect of Ambient Pressure on Nozzle Flow

F16 Missile Launch

Expandable Rocket Nozzle

Space Shuttle Nozzle AssemblyocketNozzle\SSMENozzle copy.pdf

Oblique Shock/Boundary Layer System in Supersonic Diffuser

 

     12/6   Thrust Vector Control Strategies

Solid Propellant Grain Configurations

Space Shuttle Launch Configuration Specifications

Pressurized Propellant Feed System, Hybrid and Ramjet Rockets

Cooled Rocket Thrust Chamber

Another Pressurized Propellant Feed System

Turbopump Propellant Feed System

Hydrazing Thruster with Injectors

 

     12/8     Review Notes for Final Exam

 

 

BACK TO TOP


University of Washington
Aeronautics and Astronautics