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Progress in aeronautical sciences. Volume 9 /
Progress in Aeronautical Sciences.
| Clasificación: | Libro Electrónico |
|---|---|
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés Francés |
| Publicado: |
Oxford :
Pergamon Press,
1968.
|
| Colección: | Progress in aeronautical sciences ;
v. 9. |
| Temas: | |
| Acceso en línea: | Texto completo Texto completo |
Tabla de Contenidos:
- Front Cover; Progress in Aeronautical Sciences; Copyright Page; Table of Contents; PREFACE; CHAPTER 1. LES PROC�ED�ES G�EN�ERAUX DE MESURE DES CARACT�ERISTIQUES VIBRATOIRES DES STRUCTURES LIN�EAIRES FAIBLEMENT AMORTIES; 1. D�EFINITION DES VALEURS �A MESURER; 2. PR�EPARATION ET ORGANISATION DE L'ESSAI DE VIBRATION; 3. LES PROC�ED�ES GLOBAUX DE D�ETECTION DES MODES PROPRES; 4. LES PROC�ED�ES GLOBAUX DE TRAITEMENT INDIVIDUEL DU MODE; 5. LES MOYENS D'ESSAI; 6. PERSPECTIVES; REFERENCES; CHAPTER 2. NUMERICAL METHOD OF CHARACTERISTICS FOR THREE-DIMENSIONAL SUPERSONIC FLOWS
- 1. NUMERICAL METHODS FOR SOLUTION OF THREE-DIMENSIONAL PROBLEMS IN GAS DYNAMICS2. DEVELOPMENT OF THE THREE-DIMENSIONAL METHOD OF CHARACTERISTICS; 3. FORMULATION OF THE PROBLEM AND BASIC EQUATIONS OF THE THREE-DIMENSIONAL METHOD OF CHARACTERISTICS; 4. DIRECT TETRAHEDRAL SCHEME; 5. INVERSE TETRAHEDRAL SCHEME WITH CONTINUOUS INTERPOLATIONS; 6. SCHEME USING ONLY BICHARACTERISTIC DIRECTIONS; 7. SEMI-CHARACTERISTIC SCHEME; 8. GENERALIZATION FOR THE CASE OF EQUILIBRIUM GAS FLOWS; 9. GENERALIZATION FOR THE CASE OF NON-EQUILIBRIUM GAS FLOWS; CONCLUSION; AKNOWLEDGEMENTS; REFERENCES
- CHAPTER 3. CARACT�ERISTIQUES THERMIQUES DES COUCHES LIMITES ET CALCUL PRATIQUE DES TRANSFERTS DE CHALEUR EN HYPERSONIQUEINTRODUCTION; 1. PROPRI�ET�ES ESSENTIELLES INTERVENANT AUX TEMP�ERATURES �ELEV�EES; 2. �EQUATIONS G�EN�ERALES DE LA COUCHE LIMITE EN �ECOULEMENT BIDIMENSIONNEL; 3. COUCHES LIMITES BI-DIMENSIONNELLES EN �ECOULEMENT EXT�ERIEUR UNIFORME; 4. TRANSFERTS DE CHALEUR AVEC GRADIENT DE PRESSION EN �ECOULEMENT BIDIMENSIONNEL; 5. FLUX DE CHALEUR DANS DES PROBL�EMES HYPERSONIQUES TRIDIMENSIONNELS; REFERENCES; CHAPTER 4. A REVIEW OF FLUID MECHANICAL AND RELATED PROBLEMS IN MHD GENERATORS
- PART 1. INTRODUCTION TO MHD POWER CONVERSION SYMBOLS USED IN PART 11. INTRODUCTION; 2. BASIC IDEA OF THE FARADAY GENERATOR; 3. THE HALL CURRENT AND SOME OF ITS EFFECTS; 4. GAS DYNAMICS; 5. BOUNDARY LAYERS AND VELOCITY PROFILES; 6. INSTABILITIES; 7. POSSIBLE LINES OF RESEARCH; LIST OF REFERENCES TO PART 1; PART 2. REVIEW OF SOME PAPERS PRESENTED AT A RECENT SYMPOSIUM ON M.H.D. POWER GENERATION; SYMBOLS USED IN PART 2; 1. INTRODUCTION; 2. THERMODYNAMIC CYCLE CONSIDERATIONS; 3. THE MHD DUCT IN D.C. POWER CONVERSION; 4. DUCTS WITH UNSTEADY OUTPUT; 5. SOME ENGINEERING PROBLEMS; ACKNOWLEDGEMENT
- LIST OF REFERENCES TO PART 2 (GENERAL)CHAPTER 5. AN ANALYSIS OF SOME PERFORMANCE ASPECTS OF VARIOUS TYPES OF AIRCRAFT DESIGNED TO FLY OVER DIFFERENT RANGES AT DIFFERENT SPEEDS; 1. INTRODUCTION; 2. THE OVERALL PATTERN. FIGURES OF MERIT; 3. CLASSICAL AND SWEPT TYPES OF AIRCRAFT; 4. THE SLENDER ALLWING AEROBUS; 5. SLENDER AIRCRAFT FOR SUPERSONIC FLIGHT; 6. WAVERIDER AIRCRAFT FOR HYPERSONIC FLIGHT; 7. COMPARISON BETWEEN THE VARIOUS TYPES OF AIRCRAFT; ACKNOWLEDGEMENT; REFERENCES; AUTHOR INDEX; SUBJECT INDEX