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Advances in aeronautical sciences. proceedings of the First International Congress in the Aeronautical Sciences Madrid, 8-13, September 1958 / Volume 1 :
Advances in Aeronautical Sciences.
| Clasificación: | Libro Electrónico |
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| Autor Corporativo: | |
| Otros Autores: | |
| Formato: | Electrónico Congresos, conferencias eBook |
| Idioma: | Inglés Francés Alemán |
| Publicado: |
London ; New York :
Symposium Publications Division, Pergamon Press,
1959.
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| Colección: | International series on aeronautical sciences and space flight. Symposia.
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| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Front Cover; Advances in Aeronautical Sciences; Copyright Page; Table of Contents; FOREWORD; CHAPTER 1. SOME SIGNIFICANT DEVELOPMENTS IN AERODYNAMICS SINCE 1946; WING THEORY; SLENDER WINGS AND AIRCRAFT; INTERFERENCE EFFECTS; AEROELASTIC THEORIES; NON-LINEAR THEORIES
- HIGHER-ORDER APPROXIMATIONS; TRANSONIC FLOW; HYPERSONIC FLOW; BOUNDARY LAYER THEORY; THEORY OF TURBULENCE; BIBLIOGRAPHY; CHAPTER 2. AERODYNAMIC DESIGN FOR SUPERSONIC SPEEDS; INTRODUCTION; COMPONENTS OF DRAG; MINIMUM DRAG OF LIFTING SURFACES; YAWED AND SWEPT WINGS; REDISTRIBUTION OF LIFT BY FUSELAGE; HIGH WING ARRANGEMENTS
- CANCELATION OF THICKNESS DRAGLIFT AND DRAG AT HIGH ALTITUDES; REFERENCES; DISCUSSION; CHAPTER 3. TELECOMMAND AND NAVIGATION; 1. INTRODUCTION; 2. GUIDANCE FOR THE ANTI-AIRCRAFT MISSILE; 3. GUIDANCE FOR THE BALLISTIC MISSILE AND SATELLITE VEHICLE; 4. MIXED RADIO-INERTIAL NAVIGATION SYSTEM; 5. GUIDANCE TO THE SATELLITE SPACE STATION; REFERENCES; DISCUSSION; CHAPTER 4. PROPULSION SUPERSONIQUE PAR TURBOR�EACTEURS ET PAR STATOR�EACTEURS; INTRODUCTION; 1. SCH�EMA FONDAMENTAL; 2. D�EFINITIONS PRINCIPALES; 3. EXPRESSION DE LA POUSS�EE. MACH-LIMITE; 4. ADAPTATION MUTUELLE DES �EL�EMENTS CONSTITUTIFS
- 5. R�OLE DE L,EFFICACIT�E DE LA PRISE D'AIR6. PERFORMANCES G�EN�ERALES DU STATOR�EACTEUR NORMAL; 7. �EQUIVALENCE DU STATOR�EACTEUR NORMAL ET DU TURBOR�EACTEUR �A RECHAUFFE; 8. ASSOCIATION DU STATOR�EACTEUR AU TURBOR�EACTEUR �A RECHAUFFE; 9. STATOR�EACTEUR �A D�ETONATION; 10. TURBOR�EACTEUR �A RECHAUFFE ET �A D�ERIVATION; BIBLIOGRAPHIE; ANNEXE; DISCUSSION; CHAPTER 5. NEWTONIAN FLOW THEORY IN HYPERSONIC AERODYNAMICS; REFERENCES; CHAPTER 6. DYNAMICS OF A DISSOCIATING GAS; REFERENCES; CHAPTER 7. EXPERIMENTAL INVESTIGATION OF HYPERVELOCITY FLIGHT; 1. INTRODUCTION; 2. PROBLEMS OF SIMULATION
- 3. HYPERSONIC WIND TUNNELS4. SHOCK TUBES; 5. FREE PISTON SHOCK TUNNELS; 6. ELECTRIC-ARC-DRIVEN TUNNELS; 7. LOW-DENSITY TEST FACILITIES; 8. HYPERVELOCITY RANGES; 9. FREE FLIGHT TESTING; 10. CONCLUDING REMARKS; REFERENCES; APPENDIX; CHAPTER 8. BUCKLING AND POST-BUCKLING BEHAVIOUR OF THERMALLY LOADED SKIN PANELS; NOTATION; 1. INTRODUCTION; 2. BUCKLING OF SKIN PANELS; 3. POST-BUCKLING BEHAVIOUR OF SKIN PANELS; 4. POST-BUCKLING BEHAVIOUR UNDER LONGITUDINAL COMPRESSION; 5. POST-BUCKLING BEHAVIOUR UNDER SIMULTANEOUS COMPRESSION AND SHEAR; 6. CONCLUSIONS; 7. REFERENCES; DISCUSSION
- CHAPTER 9. SOME CONTRIBUTIONS TO THE HEAT CONDUCTION AND THERMAL STRESSES ANALYSIS IN AIRCRAFT AND MISSILE STRUCTURESLIST OF SYMBOLS; SPECIAL SYMBOLS; INTRODUCTION; PART 1. A GENERAL APPROACH TO HEAT CONDUCTION PROBLEMS IN SOLIDS WITH VARIABLE AND NON-LINEAR BOUNDARY CONDITIONS; PART 2. SOLUTION OF TYPICAL PROBLEMS; APPENDIX 1 Values of the Functions Ds(pr)y Cs(pr); APPENDIX 2 Notes on the Method of ""Linearization"" for the Solution of Transcendental Equations; APPENDIX 3 Constants of Normalization; PART 3. RESULTS AND APPLICATIONS; REFERENCES