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Advances in aeronautical sciences : proceedings of the Second International Congress in the Aeronautical Sciences, Z�urich, 12-16 September 1960. Volume 3 /
Advances in Aeronautical Sciences, Volume 3 contains the proceedings of the Second International Congress in the Aeronautical Sciences held in Zurich, Switzerland, on September 12-16, 1960. The papers explore advances in aeronautical sciences and cover topics ranging from the role of entropy in the...
| Clasificación: | Libro Electrónico |
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| Autor Corporativo: | |
| Otros Autores: | |
| Formato: | Electrónico Congresos, conferencias eBook |
| Idioma: | Inglés Francés Alemán |
| Publicado: |
Oxford :
Pergamon Press,
1962.
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| Colección: | International series in aeronautics and astronautics.
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| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Front Cover; Advances in Aeronautical Sciences; Copyright Page; Table of Contents; INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES; PARTICIPATING ORGANIZATIONS; COMMITTEES AND AUTHORS; FOREWORD; CHAPTER 1. THE ROLE OF ENTROPY IN THE AERO-SPACE SCIENCES; THE WORK OF CARNOT AND CLAUSIUS; ENTHALPY AND FREE ENTHALPY; PROPULSION IN THE VOID; ENTROPY IN GAS-FLOW; ENTROPY IN BOUNDARY LAYERS; ENTROPY IN SHOCK WAVES; CONNECTIONS BETWEEN ENTROPY AND MOLECULAR THEORY; CHEMICAL EQUILIBRIUM; NON-EQUILIBRIUM STATES; ACKNOWLEDGMENTS; LITERATURE
- CHAPTER 2. POSSIBILITES ET LIMITES ACTUELLES DE LA THEORIE DES ECOULEMENTS HYPERSONIQUESI-EFFETS DE GAZ REELS; II-APPROXIMATION NEWTONIENNE; III-CALCUL DES CHOCS DETACHES; IV-ECOULEMENTS SUR DES OBSTACLES MINCES; REFERENCES; CHAPTER 3. ON THE USE OF SHOCK TUNNELS FOR RESEARCH ON HYPERSONIC FLOW; 1. INTRODUCTION; 2. THE SHOCK TUBES AND SHOCK TUNNELS AT THE NATIONAL PHYSICAL LABORATORY; 3. THE FLOW PROVIDED BY A SHOCK TUNNEL; 4. THE ESTABLISHMENT OF STEADY FLOW PAST THE MODEL UNDER TEST; 5. MEASURING TECHNIQUES; REFERENCES; DISCUSSION
- CHAPTER 4. ON THE THEORY OF HYPERSONIC FLOW OVER BLUNT-NOSED SLENDER BODIESREFERENCES; CHAPTER 5. BEITR�AGE ZUR THEORIE DER DREIDIMENSIONALEN GRENZSCHICHTEN; 1. Einleitung; 2. Die Grenzschichtgleichungen in Stromlinienkoordinaten; 3. Die integrierten Grenzschichtgleichungen; 4. Die Funktionen q und �n; 5. Das Dichteprofil und das Z�ahigkeitsprofil; 6. Die laminaren Grenzschichten; 7. Die turbulente Grenzschicht; LITERATUR; CHAPTER 6. ON THREE-DIMENSIONAL NON-LINEAR EFFECTS IN THE STABILITY OF PARALLEL FLOWS; 1. INTRODUCTION; 2. FOURIER ANALYSIS OF THE EQUATIONS OF MOTION; 3. METHOD OF SOLUTION
- 4. DISCUSSIONREFERENCES; CHAPTER 7. SOME ASPECTS OF BOUNDARY LAYER TRANSITION AT SUBSONIC SPEEDS; INTRODUCTION; TRANSITION IN THE WAKE BEHIND A FLAT PLATE; TRANSITION IN THE BOUNDARY LAYER ALONG A FLAT PLATE WITH ARTIFICIALLY INTRODUCED STREAMWISE VORTICES; TRANSITION IN THE BOUNDARY LAYER ALONG A CONCAVE PLATE; CONCLUSION; REFERENCES; CHAPTER 8. BOUNDARY LAYER TRANSITION AT THE LEADING EDGE OF THIN WINGS AND ITS EFFECT ON GENERAL NOSE SEPARATION; 1. INTRODUCTION; 2. SEPARATION PHENOMENA DEFINITIONS; 3. TRANSITION THEORIES; 4. LEADING EDGE SEPARATION; 5. CONCLUDING REMARKS; ACKNOWLEDGEMENT