The Vortex and the Jet : A Journey into the Beauty and Mystery of Flight.

Bibliographic Details
Main Author: Decher, Reiner.
Format: eBook
Language:English
Published: Singapore : Springer Singapore Pte. Limited, 2022.
Edition:1st ed.
Subjects:
Online Access:Click to View
Table of Contents:
  • Intro
  • Acknowledgements
  • A Note on Images
  • Contents
  • Abbreviations
  • 1 The Vortex-A Journey into Beauty and Mystery
  • 2 The Vortex and Wing Lift
  • 2.1 The Bound Vortex
  • 2.2 Circulation
  • 2.3 Friction to the Rescue
  • 3 Frictionless Air Cannot Provide Lift: A Paradox
  • 3.1 The Trailing Edge
  • 3.2 The Leading Edge
  • 3.3 A Better Model
  • 4 Drag, a Nightmare and a Challenge
  • 4.1 The Air Near a Surface
  • 4.1.1 The Boundary Layer Comes in Various Thicknesses
  • 4.2 How Important is Fluid Friction?
  • 4.3 Mr. Reynolds and His Number
  • 4.4 Scale Model Testing
  • 4.5 Turbulent Flow
  • 4.6 Vortex Generators
  • 5 Pressure: The Bernoulli Principle and Flow Energy Conservation
  • 5.1 Air is Compressible (Sometimes)
  • 5.1.1 An Aside: How Good is Air?
  • 5.2 Entropy (Arrrgh!@*#*!)
  • 5.3 Energy Conservation on a Streamline
  • 5.4 Enthalpy is a Property. Really? Really!
  • 5.4.1 A Few Details About Specific Heats
  • 5.5 Total Temperature
  • 5.6 Bernoulli at Last
  • 5.7 Total Pressure
  • 6 Pressure, Pressure, It's All About Pressure!
  • 6.1 Forces and Moments
  • 6.2 Data for a Simple Airfoil
  • 6.3 Calculation Iterations Toward Realism
  • 6.4 Vorticity Provides More Than Lift, It Adds to Drag!
  • 6.5 Flight in Ground Effect
  • 6.6 Dynamic Pressure and Those Convenient and Pesky Coefficients
  • 6.7 The Pitot Probe and Dynamic Pressure
  • 7 Putting It All Together
  • 7.1 Wing Lift Performance with Viscous Air
  • 7.2 Stall
  • 7.3 Why Does a Wing Stall?
  • 7.4 Adverse Pressure
  • 7.5 Transonic Flight
  • 7.6 Shock Waves
  • 7.7 Condensation at High Speed
  • 7.8 Supersonic Wings
  • 7.9 All the Airplane Aerodynamics in One Place
  • 7.10 The Computer to the Rescue
  • 7.11 Aerodynamic Heating is Not Due to Friction
  • 8 The Jet: Fluid in Motion and More Vorticity
  • 8.1 Prop Tip Vortices
  • 8.2 Jet Boundaries Are Cylindrical Sheets of Vorticity.
  • 8.3 An Aircraft Can Never Have 100% Propulsive Efficiency
  • 8.3.1 A Quantitative Aside
  • 8.4 Counter-Rotating Props
  • 9 Propulsion for Flight: Power or Thrust?
  • 9.1 The Engines: Stark Differences
  • 9.2 Limits of the Old
  • 9.2.1 The First Jet?
  • 9.3 The Gas Turbine or 'Jet' Engine
  • 9.4 Is the Gas Turbine Engine Like Another Familiar Engine?
  • 9.4.1 Yes, the Steam Engine!
  • 9.5 Energy Conservation Again, for Steady Flow Through Engines
  • 9.5.1 A Little Mathematics, Briefly
  • 9.5.2 What Happens in a Real Jet Engine?
  • 9.6 Design Issues
  • 10 The Compressor: Gas Turbine Engine Keystone
  • 10.1 Axial Flow Compressor: The Bedrock of Modern Engines
  • 10.2 Compressor Pressure Ratio
  • 10.3 Compressor Aerodynamics
  • 10.4 How Well?-Efficiency
  • 10.5 The Control Problem
  • 11 Bypass and Other Engines
  • 11.1 The Fan on a Turbofan Engine Has No IGV
  • 11.2 Bypass Ratio
  • 11.3 Turboprops and Turboshaft Engines
  • 12 Other Components of the Jet Engine
  • 12.1 The Turbine
  • 12.2 The Combustor
  • 12.3 Putting It Together into an Engine
  • 12.4 How Do You Start This Thing?
  • 12.5 Bleed Valves and Variable Stator Geometry
  • 13 More Components: Inlets, Mixers, and Nozzles
  • 13.1 Inlets
  • 13.1.1 An Old Wives' Tale About Inlets
  • 13.2 Inlet Geometry and Diverters
  • 13.3 Mixing
  • 13.4 The Nozzle
  • 13.5 Choking
  • 13.6 More Extreme Nozzles: The Rocket Engine
  • 13.6.1 Overexpansion
  • 13.6.2 Under-Expansion
  • 13.6.3 Staging
  • 13.6.4 Specific Impulse and a Little Chemistry
  • 13.7 Airplane Range
  • Epilogue
  • Appendix A Equations for Quantitative Descriptions
  • A.1 Motion with Circular Streamlines
  • A.2 Air as a Medium
  • A.3 The Descriptive Constants
  • A.4 The Gas Properties
  • A.5 The Flight Equations
  • A.6 The Equations of Aerothermodynamics
  • A.6.1 The Energy Equation Along a (Steady) Streamline
  • A.6.2 Compressibility.
  • A.6.3 Isentropic Relation Between Two States 1 and 2
  • A.6.4 Heating Total Pressure Loss
  • Appendix B Some Quantitative Aspects of Aerodynamics and Thermodynamics
  • B.1 Entropy is a Fact
  • B.2 Compressibility
  • B.3 Boundary Layers
  • Appendix C Induced Drag
  • Appendix D Aerodynamic Performance Summary
  • -4pt- Glossary of Technical Terms
  • References
  • Index.