http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
proceedings of the Second International Congress in the Aeronautical Sciences, Zürich, 12-16 September 1960
International Congress in the Aeronautical Sciences 1960 : Zürich, Switzerland)
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 aerospace sciences to the theory of hypersonic flow over blunt-nosed slender bodies. The effect of boundary layer transition at the leading edge of thin wings on general nose separation is also discussed, along with the aerodynamics of aircraft shapes for flight at supersonic speeds. This book is co.
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. BEITRÄGE ZUR THEORIE DER DREIDIMENSIONALEN GRENZSCHICHTEN; 1. Einleitung; 2. Die Grenzschichtgleichungen in Stromlinienkoordinaten; 3. Die integrierten Grenzschichtgleichungen; 4. Die Funktionen q und ñ; 5. Das Dichteprofil und das Zähigkeitsprofil; 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
editorial committee: Chairman: Th. von Kármán.
Advances in Aeronautical Sciences : Proceedings of the Second International Congress in the Aeronautical Sciences, Zürich, 12-16 September 1960
International series in aeronautics and astronautics