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[null,"1.","Record Nr.",null,"UNISA990003679170203316"]
[null,null,"Autore",null,"ZAOUCHI-RAZGALLAH, Rawdha"]
[null,null,"Titolo",null,"La scrittura fantastica di Giuseppe Bonaviri / Rawdha Zaouchi-Razgallah ; con l'introduzione di Sarah Zappulla Muscarà"]
[null,null,"Pubbl/distr/stampa",null,"Floridia ; Roma : Sampognaro & Pupi, 2012"]
[null,null,"ISBN",null,"978-88-95760-25-4"]
[null,null,"Descrizione fisica",null,"208 p. : ill. ; 20 cm"]
[null,null,"Disciplina",null,"853.914"]
[null,null,"Soggetti",null,"Bonaviri, Giuseppe"]
[null,null,"Collocazione",null,"VI.3.B. 4317"]
[null,null,"Lingua di pubblicazione",null,"Italiano"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,"2.","Record Nr.",null,"UNINA9910457232503321"]
[null,null,"Titolo",null,"Thermophysical aspects of re-entry flows [[electronic resource] /] / edited by James N. Moss, Carl D. Scott"]
[null,null,"Pubbl/distr/stampa",null,"New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986"]
[null,null,"ISBN",null,"1-60086-577-1"]
[{"$nulls":4},"1-60086-358-2"]
[null,null,"Descrizione fisica",null,"1 online resource (636 p.)"]
[null,null,"Collana",null,"Progress in astronautics and aeronautics ; ; v. 103"]
[null,null,"Disciplina",null,"629.1 s"]
[{"$nulls":4},"629.4/152"]
[null,null,"Soggetti",null,"Space vehicles - Atmospheric entry"]
[{"$nulls":4},"Aerothermodynamics"]
[{"$nulls":4},"Aerodynamics, Hypersonic"]
[{"$nulls":4},"Electronic books."]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","\"Technical papers selected from the AIAA 23rd Aerospace Sciences Meeting, January 1985, and the AIAA 20th Thermophysics Conference, June 1985, and subsequently revised.\""]
[null,null,null,"Nota di bibliografia","Includes bibliographical references and index."]
[null,null,"Nota di contenuto",null,"\"\"Cover\"\"; \"\"Title\"\"; \"\"Copyright\"\"; \"\"Table of Contents\"\"; \"\"Preface\"\"; \"\"Editorial Committee\"\"; \"\"Chapter I. Low-Density Phenomena\"\"; \"\"Low-Density Aerothermodynamics\"\"; \"\"Direct Simulation Monte Carlo Method and Comparison with Experiment\"\"; \"\"Drag of Bodies in Rarefied Hypersonic Flow\"\"; \"\"Heat Transfer on a Flat Plate in Continuum to Rarefied Hypersonic Flows at Mach 19.2 and 25.4\"\"; \"\"Transitional, Hypervelocity Aerodynamic Simulation and Scaling\"\"; \"\"Gas/Surface Scattering Models for Satellite Applications\"\"; \"\"Chapter II. High Temperature Kinetics and Transport Properties\"\""]
[{"$nulls":4},"\"\"Rate Constants for Chemical Reactions in High-Temperature Nonequilibrium Air\"\"\"\"Electron-Nitrogen Molecule Collisions in High-Temperature Nonequilibrium Air\"\"; \"\"Electron-Impact Vibrational Excitation Rates in the Flowfield of Aeroassisted Orbital Transfer Vehicles\"\"; \"\"Theoretical Studies of Dissociative Recombination\"\"; \"\"N+ -N and 0+ -0 Interaction Energies, Dipole Transition Moments, and Transport Cross Sections\"\"; \"\"Transport Properties for Some Atom/Ion Interactions in Air\"\"; \"\"Chapter III. Aerothermodynamic Ground Simulations and Measurements\"\""]
[{"$nulls":4},"\"\"Studies of Potential Fluid-Mechanical Mechanisms for Enhanced Stagnation-Region Heating\"\"\"\"Measured and Predicted Vortex-Induced Leeward Heating on a Biconic at Mach 6 and 10\"\"; \"\"Heating Rate Distributions at Mach 10 on a Circular-Body Earth-to-Orbit Transport Vehicle\"\"; \"\"Developments in Aerothermal Test Techniques at the AEDC Supersonic/Hypersonic Wind Tunnels\"\"; \"\"Application of Numerical Simulation to Enhance Arcjet Performance\"\"; \"\"Effects of Surface Discontinuities on Convective Heat Transfer in Hypersonic Flow\"\"; \"\"Chapter IV. Numerical Simulations of Hypersonic Flows\"\""]
[{"$nulls":4},"\"\"Chemical and Thermal Nonequilibrium Heat-Transfer Analysis for Hypervelocity,Low Reynolds Number Flow\"\"\"\"Convergence of Computation of Chemical Reacting Flows\"\"; \"\"Radiative Viscous Shock Layer Analysis of Fire,Apollo, and PAET Flight Data\"\"; \"\"Three-Dimensional Viscous Shock Layer Applications for the Space Shuttle Orbiter\"\"; \"\"Numerical Simulation of Hypersonic Viscous Fore- and Afterbody Flows over Capsule-Type Vehicles at Angles of Attack\"\"; \"\"Two Dimensional and Axisymmetric Heat-Transfer Results with the CSCM Upwind Implicit Algorithm\"\"; \"\"Author Index\"\""]