Küchemann / Carrière / Rott Progress in Aeronautical Sciences

1. Auflage 2014
ISBN: 978-1-4832-2488-6
Verlag: Elsevier Science & Techn.
Format: PDF
Kopierschutz: 1 - PDF Watermark

E-Book, Englisch, Band Volume 9, 480 Seiten, Web PDF

Reihe: Progress in Aeronautical Sciences

Progress in Aeronautical Sciences, Volume 9 presents the vibrational characteristics of certain aircraft. This book supplements the comprehensive account of matrix methods of structural analysis. Organized into five chapters, this volume begins with an overview of the different schemes of the numerical method of characteristics for calculating three-dimensional steady supersonic gas flow about bodies moving at incidence. This text then examines the flow of a perfect gas and provides the generalization for the case of equilibrium and non-equilibrium flow of real gas. Other chapters consider the various aspects of the aerodynamic design of aircraft and discuss the application of modern computer methods to fluid mechanics. This book discusses as well the prospects for further development of the existing types and for the establishment of the as yet hypothetical types of aircraft. The final chapter shows how the evolution of the aerodynamic shape leads to a complete spectrum of major types of aircraft. This book is a valuable resource for engineers.

Autoren/Hrsg.

Küchemann, D.

Carrière, P.

Rott, N.

Inhaltsverzeichnis

1;Front Cover;1
2;Progress in Aeronautical Sciences;4
3;Copyright Page;5
4;Table of Contents;6
5;PREFACE;8
6;CHAPTER 1. LES PROCÉDÉS GÉNÉRAUX DE MESURE DES CARACTÉRISTIQUES VIBRATOIRES DES STRUCTURES LINÉAIRES FAIBLEMENT AMORTIES;10
6.1;1. DÉFINITION DES VALEURS À MESURER;11
6.2;2. PRÉPARATION ET ORGANISATION DE L'ESSAI DE VIBRATION;15
6.3;3. LES PROCÉDÉS GLOBAUX DE DÉTECTION DES MODES PROPRES;17
6.4;4. LES PROCÉDÉS GLOBAUX DE TRAITEMENT INDIVIDUEL DU MODE;25
6.5;5. LES MOYENS D'ESSAI;44
6.6;6. PERSPECTIVES;47
6.7;REFERENCES;47
7;CHAPTER 2. NUMERICAL METHOD OF CHARACTERISTICS FOR THREE-DIMENSIONAL SUPERSONIC FLOWS;50
7.1;1. NUMERICAL METHODS FOR SOLUTION OF THREE-DIMENSIONAL PROBLEMS IN GAS DYNAMICS;50
7.2;2. DEVELOPMENT OF THE THREE-DIMENSIONAL METHOD OF CHARACTERISTICS;57
7.3;3. FORMULATION OF THE PROBLEM AND BASIC EQUATIONS OF THE THREE-DIMENSIONAL METHOD OF CHARACTERISTICS;66
7.4;4. DIRECT TETRAHEDRAL SCHEME;73
7.5;5. INVERSE TETRAHEDRAL SCHEME WITH CONTINUOUS INTERPOLATIONS;82
7.6;6. SCHEME USING ONLY BICHARACTERISTIC DIRECTIONS;91
7.7;7. SEMI-CHARACTERISTIC SCHEME;100
7.8;8. GENERALIZATION FOR THE CASE OF EQUILIBRIUM GAS FLOWS;111
7.9;9. GENERALIZATION FOR THE CASE OF NON-EQUILIBRIUM GAS FLOWS;119
7.10;CONCLUSION;127
7.11;AKNOWLEDGEMENTS;127
7.12;REFERENCES;127
8;CHAPTER 3. CARACTÉRISTIQUES THERMIQUES DES COUCHES LIMITES ET CALCUL PRATIQUE DES TRANSFERTS DE CHALEUR EN HYPERSONIQUE;132
8.1;INTRODUCTION;134
8.2;1. PROPRIÉTÉS ESSENTIELLES INTERVENANT AUX TEMPÉRATURES ÉLEVÉES;135
8.3;2. ÉQUATIONS GÉNÉRALES DE LA COUCHE LIMITE EN ÉCOULEMENT BIDIMENSIONNEL;145
8.4;3. COUCHES LIMITES BI-DIMENSIONNELLES EN ÉCOULEMENT EXTÉRIEUR UNIFORME;158
8.5;4. TRANSFERTS DE CHALEUR AVEC GRADIENT DE PRESSION EN ÉCOULEMENT BIDIMENSIONNEL;199
8.6;5. FLUX DE CHALEUR DANS DES PROBLÈMES HYPERSONIQUES TRIDIMENSIONNELS;209
8.7;REFERENCES;221
9;CHAPTER 4. A REVIEW OF FLUID MECHANICAL AND RELATED PROBLEMS IN MHD GENERATORS;224
9.1;PART 1. INTRODUCTION TO MHD POWER CONVERSION SYMBOLS USED IN PART 1;224
9.1.1;1. INTRODUCTION;226
9.1.2;2. BASIC IDEA OF THE FARADAY GENERATOR;227
9.1.3;3. THE HALL CURRENT AND SOME OF ITS EFFECTS;233
9.1.4;4. GAS DYNAMICS;239
9.1.5;5. BOUNDARY LAYERS AND VELOCITY PROFILES;244
9.1.6;6. INSTABILITIES;256
9.1.7;7. POSSIBLE LINES OF RESEARCH;257
9.1.8;LIST OF REFERENCES TO PART 1;259
9.2;PART 2. REVIEW OF SOME PAPERS PRESENTED AT A RECENT SYMPOSIUM ON M.H.D. POWER GENERATION;262
9.2.1;SYMBOLS USED IN PART 2;262
9.2.2;1. INTRODUCTION;265
9.2.3;2. THERMODYNAMIC CYCLE CONSIDERATIONS;266
9.2.4;3. THE MHD DUCT IN D.C. POWER CONVERSION;286
9.2.5;4. DUCTS WITH UNSTEADY OUTPUT;316
9.2.6;5. SOME ENGINEERING PROBLEMS;325
9.2.7;ACKNOWLEDGEMENT;331
9.2.8;LIST OF REFERENCES TO PART 2 (GENERAL);332
10;CHAPTER 5. AN ANALYSIS OF SOME PERFORMANCE ASPECTS OF VARIOUS TYPES OF AIRCRAFT DESIGNED TO FLY OVER DIFFERENT RANGES AT DIFFERENT SPEEDS;338
10.1;1. INTRODUCTION;341
10.2;2. THE OVERALL PATTERN. FIGURES OF MERIT;342
10.3;3. CLASSICAL AND SWEPT TYPES OF AIRCRAFT;346
10.4;4. THE SLENDER ALLWING AEROBUS;371
10.5;5. SLENDER AIRCRAFT FOR SUPERSONIC FLIGHT;391
10.6;6. WAVERIDER AIRCRAFT FOR HYPERSONIC FLIGHT;413
10.7;7. COMPARISON BETWEEN THE VARIOUS TYPES OF AIRCRAFT;442
10.8;ACKNOWLEDGEMENT;460
10.9;REFERENCES;460
11;AUTHOR INDEX;466
12;SUBJECT INDEX;472