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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 |
|---|---|
| Autor Corporativo: | |
| Otros Autores: | |
| 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: | |
| Acceso en línea: | Texto completo |
MARC
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| 111 | 2 | |a International Congress in the Aeronautical Sciences |n (1st : |d 1958 : |c Madrid, Spain) | |
| 245 | 1 | 0 | |a Advances in aeronautical sciences. |n Volume 1 : |b proceedings of the First International Congress in the Aeronautical Sciences Madrid, 8-13, September 1958 / |c editorial Committee: Chairman, Th. von K�arm�an [and others]. |
| 246 | 3 | |a Aeronautical sciences | |
| 260 | |a London ; |a New York : |b Symposium Publications Division, Pergamon Press, |c 1959. | ||
| 300 | |a 1 online resource : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a International series on aeronautical sciences and space flight. Division IX, Symposia | |
| 504 | |a Includes bibliographical references. | ||
| 588 | 0 | |a Online resource; title from PDF title page (EBSCO, viewed February 6, 2015). | |
| 546 | |a Text in English, French or German. | ||
| 505 | 0 | |a 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 | |
| 505 | 8 | |a 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 | |
| 505 | 8 | |a 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 | |
| 505 | 8 | |a 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 | |
| 505 | 8 | |a 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 | |
| 520 | |a Advances in Aeronautical Sciences. | ||
| 650 | 0 | |a Aeronautics |v Congresses. | |
| 650 | 0 | |a Astronautics |v Congresses. | |
| 650 | 6 | |a A�eronautique |0 (CaQQLa)201-0000392 |v Congr�es. |0 (CaQQLa)201-0378219 | |
| 650 | 6 | |a Astronautique |0 (CaQQLa)201-0000399 |v Congr�es. |0 (CaQQLa)201-0378219 | |
| 650 | 7 | |a TECHNOLOGY & ENGINEERING |x Engineering (General) |2 bisacsh | |
| 650 | 7 | |a Aeronautics |2 fast |0 (OCoLC)fst00798293 | |
| 650 | 7 | |a Astronautics |2 fast |0 (OCoLC)fst00819505 | |
| 655 | 2 | |a Congress |0 (DNLM)D016423 | |
| 655 | 7 | |a proceedings (reports) |2 aat |0 (CStmoGRI)aatgf300027316 | |
| 655 | 7 | |a Conference papers and proceedings |2 fast |0 (OCoLC)fst01423772 | |
| 655 | 7 | |a Conference papers and proceedings. |2 lcgft | |
| 655 | 7 | |a Actes de congr�es. |2 rvmgf |0 (CaQQLa)RVMGF-000001049 | |
| 700 | 1 | |a Von K�arm�an, Theodore, |d 1881-1963. | |
| 776 | 0 | 8 | |i Print version: |a Von K�arm�an, Th. |t Advances in Aeronautical Sciences : Proceedings of the First International Congress in the Aeronautical Sciences, Madrid, 8-13 September 1958. |d Burlington : Elsevier Science, �2014 |z 9781483198323 |
| 830 | 0 | |a International series on aeronautical sciences and space flight. |n Division IX, |p Symposia. | |
| 856 | 4 | 0 | |u https://sciencedirect.uam.elogim.com/science/book/9781483198323 |z Texto completo |