Acknowledgements
|
1 |
Foreword
|
4 |
|
|
8 |
PART ONE—Theory, Applications and Design Procedure
|
|
|
10 |
-
Why a Duct?
-
Applications
-
...and Why Not
|
Basic Propulsion Physics
|
18 |
-
Force and Momentum
-
Where Thrust Comes From
-
Power Required to Generate Thrust
-
Maximizing Thrust per Horsepower
-
Propulsive Efficiency
|
|
|
23 |
-
Copying Turbojet Inlets
-
Copying Turbofan Inlets
-
High Pressure Ratios
-
Unrealistic Performance Goals
-
Ignoring Powerplant Limitations
-
Inlet Design; Cheater Holes, Blow-In Doors and Other Atrocities
-
Fan Placement: Inlet, Throat or Exit?
-
Boundary Layer Ingestion vs Boundary Layer Bleed or Diversion
|
Duct Nomenclature and Design Principles
|
30 |
-
Nomenclature
-
The Engineering Model of the Duct
-
Relations used in duct design
-
Velocity Change and Pressure Rise
|
Duct Design Procedure
|
34 |
-
Tools
-
Outline of the Design Method
-
Estimate of Stage and Duct Efficiency
-
Engine Rating
-
Preliminary Fan Sizing
-
Mass Flow—First Estimate
-
Capture Area
-
Fan Entry Static Pressure
-
Fan Flow Speed
-
Duct Exit
-
Fan Swirl Parameter; Swirl Horsepower
-
Accounting for Swirl
-
Fan Delivery Pressure
-
Check: Power Required
-
Iteration: New Mass Flow Estimate
-
Tip Mach Number Check
-
Longitudinal Duct Profile
-
Duct Cross-Section Shapes
-
Bends
-
Inlet Design
|
Fan Design
|
47 |
-
Design Method
-
Design Procedure—Blade Twist Distribution
-
Optimum Fan Blade Design
-
A Simple Stator—The NPL Straightener
|
Static Thrust Estimation
|
58 |
-
Method I: Constant Mass Flow and Power
-
Method II: ACV Correlation Line
|
PART TWO— Engines, Fans and Aircraft
|
Engines
|
62 |
-
Operating Cycles
-
Power Output
-
Available Engines
|
Ducted Fan Aircraft
|
82 |
-
VTOL Aircraft Using Tilt-ducts
-
Flying Platforms Using Ducted Propellers/Fans
-
The Flying Jeeps
-
"Tunnel" Aircraft
|
PART THREE—Bibliography and Symbol Table
|
Bibliography
|
140 |
-
Report Series and Sources
|
Symbols
|
164 |
PART FOUR—Design Example
|
Duct Design Example
|
166 |
Fan Design Example
|
169 |