Advances in aeronautical sciences. proceedings of the First International Congress in the Aeronautical Sciences Madrid, 8-13, September 1958 / Volume 2 :

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Advances in Aeronautical Sciences.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor Corporativo: International Congress in the Aeronautical Sciences Madrid, Spain
Otros Autores: Von K�arm�an, Theodore, 1881-1963
Formato: Electrónico Congresos, conferencias eBook
Idioma:Inglés
Francés
Alemán
Publicado: London ; New York : Symposium Publications Division, Pergamon Press, 1959.
Colección:International series on aeronautical sciences and space flight. Symposia.
Temas:
Aeronautics > Congresses.
Astronautics > Congresses.
A�eronautique > Congr�es.
Astronautique > Congr�es.
TECHNOLOGY & ENGINEERING > Engineering (General)
Aeronautics
Astronautics
Congress
proceedings (reports)
Conference papers and proceedings
Conference papers and proceedings.
Actes de congr�es.
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Front Cover; Advances in Aeronautical Sciences; Copyright Page; Table of Contents; FOREWORD; CHAPTER 1. EINIGE NEUERE ERGEBNISSE �UBER GRENZSCHICHTBEEINFLUSSUNG; 1. EINLEITUNG; 2. BERECHNUNG DER TURBULENTEN GRENZSCHICHT MIT ABSAUGUNG UND AUSBLASEN; 3. STABILIT�AT DER LAMINAREN GRENZSCHICHT MIT SCHLITZABSAUGUNG; 4. UNTERSUCHUNGEN AN GRENZSCHICHTZ�AUNEN; 5. ZUSAMMENFASSUNG; 6. LITERATUR; DISCUSSION; CHAPTER 2. FUNDAMENTAL DESIGN PROBLEMS OF AIRCRAFT WITH BOUNDARY LAYER CONTROL FOR MAINTAINING LAMINAR FLOW; INTRODUCTION; 1. THE STATE OF THE ART; 2. ENGINEERING CONSIDERATIONS
  • 3. POTENTIAL APPLICATIONS OF BOUNDARY LAYER CONTROL FOR LOW DRAGAPPENDIX I: BOUNDARY LAYER FLIGHT RESEARCH IN GREAT BRITAIN AND IN THE U.S.A. 1952-1957; APPENDIX II: AN APPROXIMATE METHOD FOR CALCULATING CROSS-FLOW ON AN INFINITE SWEPT WING WITH ARBITRARY VELOCITY AND SUCTION DISTRIBUTIONS; APPENDIX III: PERFORMANCE ASPECTS; REFERENCES; DISCUSSION; CHAPTER 3. CONTRIBUTION TH�EORIQUE ET EXPERIMENTALE �A L'ETUDE DU CONTR�OLE DE LA COUCHE LIMITE PAR SOUFFLAGE; NOTATIONS; INTRODUCTION; 1. ANALYSE EXP�ERIMENTALE DE L'�ECOULEMENT AU VOISINAGE DE LA PAROI; 2. INTERPRETATION TH�EORIQUE DES RESULTATS
  • 9. COMPARISON OF CL VALUES WITH THOSE OBTAINED BY OTHER METHODS10. CONCLUDING REMARKS; REFERENCES; DISCUSSION; CHAPTER 5. AEROELASTIC PROBLEMS ON AIRCRAFT CONSTRUCTION; 1. INTRODUCTION; 2. THE KINDS OF AEROELASTIC PHENOMENA; 3. CONSTRUCTIONAL MEASURES TO PREVENT NOXIOUS AEROELASTIC PHENOMENA; 4. METHODS FOR SOLVING AEROELASTIC PROBLEMS AT THE DEVELOPMENT OF PROTOTYPE AIRCRAFT; REFERENCES; CHAPTER 6. A REVIEW OF SOME RECENT DEVELOPMENTS IN HYPERSONIC FLOW; INTRODUCTION; 1. CHEMICAL-PHYSICAL EFFECTS; 2. DETERMINATION OF THE PRESSURE DISTRIBUTION; 3. HEAT TRANSFER; 4. ENTROPY EFFECTS
  • 5. CONCLUSIONSREFERENCES; CHAPTER 7. PROBLEMES DE L'AILE ANNULAIR�E RESOLUS PAR ANALOGIE RHEOELECTRIQUE; INTRODUCTION; AILE ANNULAIRE DANS L'ECOULEMENT A SYMETRIE AXIALE; AILE ANNULAIRE EN INCIDENCE; CONCLUSION; REFERENCES; DISCUSSION; CHAPTER 8. EINIGE ERGEBNISSE AUS DER THEORIE DES RINGFL�UGELS IN INKOMPRESSIBLER STR�OMUNG; EINLEITUNG UND �UBERSICHT; 1. REIBUNGSLOSE STR�OMUNG; 2. GRENZSCHICHT UND WIDERSTAND; SCHLUSSBEMERKUNGEN; SCHRIFTTUM; DISCUSSION; CHAPTER 9. A CONTRIBUTION TO THE SOLUTION OF MIXED PROBLEMS OF TRANSONIC AERODYNAMICS; INTRODUCTION; DESCRIPTION OF THE METHOD

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