Progress in Aeronautical Sciences ：Volume 8

Publication subTitle ：Volume 8

Author： Küchemann D.;Carrière P.;Etkin B.

Publisher： Elsevier Science‎

Publication year： 2016

E-ISBN: 9781483149080

P-ISBN(Paperback): 9780080120409

Subject：

Keyword：一般工业技术

Language： ENG

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Description

Progress in Aeronautical Sciences, Volume 8 is a collection of papers that covers the widening field of aeronautical sciences.
The first article deals with problems in fluid mechanics and practical aerodynamics. This paper includes reducing problems to integral equations; the comparison of calculated results with exact analytic solutions; and with experimental pressure distributions using various configurations. The book follows this discussion with a review of the methods for designing swept-winged aircraft, including the design of a symmetrical-fuselage combination at zero incidence.
The text also reviews the propulsion characteristics of a hypothetical aircraft flying at hypersonic speeds, and then focuses on air-breathing engines to power hypersonic aircrafts of which the scramjet is the most promising. The publication renders a comprehensive report on the viscous flow in boundary layers in ducts under rarefied conditions. The book then reviews investigations made on the viscous flow through tubes, both in continuum flow and in free-molecule flow. Another paper develops the fundamental mathematical and physical bases of magnetohydrodynamic flow through ducts in the presence of an applied electromagnetic field. Such review is useful when applied to electromagnetic flowmeters, pumps, or generators.
The volume can be helpful for aerodynamic researchers, aviation technologists and designers, and aeronautical engineers.

Chapter

Front Cover

Progress in Aeronautical Sciences

Table of Contents

Preface

Chapter 1. Calculation of Potential Flow about Arbitrary Bodies

PRINCIPAL NOTATION

1. INTRODUCTION

2. REDUCTION OF THE PROBLEM TO AN INTEGRAL EQUATION FOR A SOURCE-DENSITY DISTRIBUTION ON THE BODY SURFACE

3. THE METHOD OF SOLUTION

4. CALCULATION OF THE POTENTIAL AND VELOCITY INDUCED BY A SURFACE ELEMENT AT A POINT IN SPACE

5. SOLUTION OF THE LINEAR ALGEBRAIC EQUATIONS FOR THE VALUES OF THE SURFACE SOURCE DENSITY

6. OTHER EXACT NUMERICAL METHODS OF SOLUTION

7. COMPARISON OF CALCULATED VELOCITY DISTRIBUTIONS WITH EXACT ANALYTIC SOLUTIONS

8. COMPARISON OF CALCULATED AND EXPERIMENTAL PRESSURE DISTRIBUTIONS ON VARIOUS CONFIGURATIONS

9. CALCULATED FLOWS ABOUT CERTAIN BODIES

10. OTHER PHYSICAL PROBLEMS

REFERENCES

Chapter 2. Theory of Aerodynamic Design for Swept-winged Aircraft at Transonic and Supersonic Speeds

PRINCIPAL SYMBOLS

1. INTRODUCTION

2. BASIC PHYSICAL PRINCIPLES

3. GENERAL DESIGN PROCEDURE

4. DESIGN OF A SYMMETRICAL-FUSELAGE COMBINATION AT ZERO INCIDENCE

5. DESIGN OF THE WINGS AND FUSELAGE FOR LIFTING CONDITIONS

6. SUMMARY OF THE RECOMMENDED DESIGN METHOD

7. CONCLUDING REMARKS

ACKNOWLEDGEMENTS

APPENDIX I

APPENDIX II

APPENDIX III

REFERENCES

CHAPTER 3. Hypersonic Air-breathing Propulsion

LIST OF SYMBOLS

1.0 INTRODUCTION

2.0 HISTORICAL DEVELOPMENT

3.0 THEORETICAL CYCLE ANALYSIS

3.1 APPROXIMATE ANALYSIS

3.2 EXACT ANALYSIS

4.0 SYSTEM STUDIES

4.1 CRUISE VEHICLES

4.2 BOOST VEHICLES

5.0 INTAKES

6.0 SUPERSONIC COMBUSTION AND MIXING

7.0 EXHAUST NOZZLE

CURRENT POSITION

ACKNOWLEDGEMENTS

REFERENCES

CHAPTER 4. Boundary Layers in Rarefied Gas Flow

NOTATION

1. INTRODUCTION

2. ELEMENTS OF KINETIC THEORY

3. COMPARISONS BETWEEN EXPERIMENT AND KINETIC THEORY FOR RAREFIED GASES

4. SPECIAL VISCOUS FLOW PROBLEMS

5. THE BOUNDARY-LAYER EQUATION IN SLIP FLOW

6. VISCOUS FLOW IN TUBES AND CHANNELS

7. BOUNDARY-LAYER CONTROL

REFERENCES

CHAPTER 5.Magnetohydrodynamic Channel Flow

SYMBOLS

1. INTRODUCTION

2. MAGNETOGASDYNAMIC EQUATIONS

3. FULLY DEVELOPED CHANNEL FLOW

4. FULLY DEVELOPED CHANNEL FLOW—FINITECROSS-SECTION

5. ENTRY PROBLEM

6. HALL EFFECT

7. SUMMARY

ACKNOWLEDGMENTS

REFERENCES

Auther Index

Subject Index

Contents of Previous Volumes

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