Aerodynamics for aviators / / Mark Dusenbury, Gary Ullrich, Shelby Balogh |
Autore | Dusenbury Mark |
Edizione | [Second edition.] |
Pubbl/distr/stampa | Newcastle, Washington : , : Aviation Supplies & Academics, Inc., , 2016 |
Descrizione fisica | 1 online resource (ix, 230 pages) |
Disciplina | 629.1323 |
Soggetto topico |
Aerodynamics
Airplanes - Piloting Airplanes - Performance |
ISBN | 1-61954-334-6 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910817569703321 |
Dusenbury Mark
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Newcastle, Washington : , : Aviation Supplies & Academics, Inc., , 2016 | ||
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Lo trovi qui: Univ. Federico II | ||
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Aerodynamics for engineering students / E. L. Houghton, P. W. Carpenter |
Autore | Houghton, Edward L. |
Edizione | [4th ed] |
Pubbl/distr/stampa | London : Arnold, 1993 |
Descrizione fisica | XIII, 515 p. ; 24 cm. |
Disciplina | 629.1323 |
Altri autori (Persone) | Carpenter, Peter W. |
ISBN | 03-405-4847-9 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNICAMPANIA-SUN0035679 |
Houghton, Edward L.
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London : Arnold, 1993 | ||
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Lo trovi qui: Univ. Vanvitelli | ||
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Aerodynamics for engineering students / E. L. Houghton, P. W. Carpenter |
Autore | Houghton, Edward L. |
Edizione | [4th ed] |
Pubbl/distr/stampa | London, : Arnold, 1993 |
Descrizione fisica | XIII, 515 p. ; 24 cm |
Disciplina | 629.1323 |
Altri autori (Persone) | Carpenter, Peter W. |
ISBN | 03-405-4847-9 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Titolo uniforme | |
Record Nr. | UNICAMPANIA-VAN0035679 |
Houghton, Edward L.
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London, : Arnold, 1993 | ||
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Lo trovi qui: Univ. Vanvitelli | ||
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Aerodynamics for engineering students [e-book] / E.L. Houghton and P.W. Carpenter |
Autore | Houghton, E. L. (Edward Lewis) |
Edizione | [5th ed.] |
Pubbl/distr/stampa | Oxford ; Boston : Butterworth-Heinemann, c2003 |
Descrizione fisica | xiv, 590 p. : ill. ; 25 cm |
Disciplina | 629.1323 |
Altri autori (Persone) | Carpenter, Peter William, 1942- |
Altri autori (Enti) | Elsevier Science Publishers |
Soggetto topico |
Aerodynamics
Airplanes - Design and construction |
Soggetto genere / forma | Electronic books. |
Formato | Risorse elettroniche ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Basic concepts and definitions -- Governing equations of fluid mechanics -- Potential flow -- Two-dimensional wing theory -- Finite wing theory -- Compressible flow -- Viscous flow and boundary layers -- Flow control and wing design -- Propellers and propulsion |
Record Nr. | UNISALENTO-991003224429707536 |
Houghton, E. L. (Edward Lewis)
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Oxford ; Boston : Butterworth-Heinemann, c2003 | ||
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Lo trovi qui: Univ. del Salento | ||
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Aerodynamics for engineers / / John J. Bertin and Russell M. Cummings ; international edition contributions by P. Venkata Reddy |
Autore | Bertin John J. <1938-> |
Edizione | [Sixth edition, International edition.] |
Pubbl/distr/stampa | Boston : , : Pearson, , [2014] |
Descrizione fisica | 1 online resource (832 pages) : illustrations, photographs, tables |
Disciplina | 629.1323 |
Collana | Always learning |
Soggetto topico | Aerodynamics |
ISBN | 0-273-79352-7 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Cover -- Aerodynamics for Engineers -- Contents -- Preface -- Why Study Aerodynamics? -- Aerodynamics and the Energy-Maneuverability Technique -- Solving for the Aerothermodynamic Parameters -- Description of an Airplane -- Summary -- Problems -- References -- Fundamentals of Fluid Mechanics -- Introduction to Fluid Dynamics -- Conservation of Mass -- Conservation of Linear Momentum -- Applications to Constant-Property Flows -- Reynolds Number and Mach Number as Similarity Parameters -- Concept of the Boundary Layer -- Conservation of Energy -- First Law of Thermodynamics -- Derivation of the Energy Equation -- Summary -- Problems -- References -- Dynamics of an Incompressible, Inviscid Flow Field -- Inviscid Flows -- Bernoulli's Equation -- Use of Bernoulli's Equation to Determine Airspeed -- The Pressure Coefficient -- Circulation -- Irrotational Flow -- Kelvin's Theorem -- Incompressible, Irrotational Flow and the Velocity Potential -- Stream Function in a Two-Dimensional, Incompressible Flow -- Relation between Streamlines and Equipotential Lines -- Superposition of Flows -- Elementary Flows -- Adding Elementary Flows to Describe Flow Around a Cylinder -- Lift and Drag Coefficients as Dimensionless Flow-Field Parameters -- Flow Around a Cylinder with Circulation -- Source Density Distribution on the Body Surface -- Incompressible, Axisymmetric Flow -- Summary -- Problems -- References -- Viscous Boundary Layers -- Equations Governing the Boundary Layer for a Steady, Two-dimensional, Incompressible Flow -- Boundary Conditions -- Incompressible, Laminar Boundary Layer -- Boundary-Layer Transition -- Incompressible, Turbulent Boundary Layer -- Eddy Viscosity and Mixing Length Concepts -- Integral Equations for a Flat-Plate Boundary Layer -- Thermal Boundary Layer for Constant-Property Flows -- Summary -- Problems -- References.
Characteristic Parameters for Airfoil and Wing Aerodynamics -- Characterization of Aerodynamic Forces and Moments -- Airfoil Geometry Parameters -- Wing-Geometry Parameters -- Aerodynamic Force and Moment Coefficients -- Wings of Finite Span -- Problems -- References -- Incompressible Flows Around Airfoils of Infinite Span -- General Comments -- Circulation and the Generation of Lift -- General Thin-Airfoil Theory -- Thin, Flat-Plate Airfoil (Symmetric Airfoil) -- Thin, Cambered Airfoil -- Laminar-Flow Airfoils -- High-Lift Airfoil Sections -- Multielement Airfoil Sections for Generating High Lift -- High-Lift Military Airfoils -- Summary -- Problems -- References -- Incompressible Flow About Wings of Finite Span -- General Comments -- Vortex System -- Lifting-Line Theory for Unswept Wings -- Panel Methods -- Vortex Lattice Method -- Factors Affecting Drag Due-to-Lift at Subsonic Speeds -- Delta Wings -- Leading-Edge Extensions -- Asymmetric Loads on the Fuselage at High Angles of Attack -- Flow Fields for Aircraft at High Angles of Attack -- Unmanned Air Vehicle Wings -- Summary -- Problems -- References -- Dynamics of a Compressible Flow Field -- Thermodynamic Concepts -- Adiabatic Flow in a Variable-Area Streamtube -- Isentropic Flow in a Variable-Area Streamtube -- Converging-diverging Nozzles -- Characteristic Equations and Prandtl-Meyer Flows -- Shock Waves -- Viscous Boundary Layer -- Shock-Wave/Boundary-Layer Interactions -- Shock/Shock Interactions -- The Role of Experiments for Generating Information Defining the Flow Field -- Comments About the Scaling/Correction Process(es) for Relatively Clean Cruise Configurations -- Summary -- Problems -- References -- Compressible, Subsonic Flows and Transonic Flows -- Compressible, Subsonic Flow -- Transonic Flow Past Unswept Airfoils -- Wave Drag Reduction by Design. Swept Wings at Transonic Speeds -- Transonic Aircraft -- Summary -- Problems -- References -- Two-Dimensional, Supersonic Flows Around Thin Airfoils -- Linear Theory -- Second-Order Theory (Busemann's Theory) -- Shock-Expansion Technique -- Summary -- Problems -- References -- Supersonic Flows Over Wings and Airplane Configurations -- General Remarks About Lift and Drag -- General Remarks About Supersonic Wings -- Governing Equation and Boundary Conditions -- Consequences of Linearity -- Solution Methods -- Conical-Flow Method -- Singularity-Distribution Method -- Design Considerations for Supersonic Aircraft -- Some Comments About the Design of the SST and of the HSCT -- Slender Body Theory -- Base Drag -- Aerodynamic Interaction -- Aerodynamic Analysis for Complete Configurations in a Supersonic Free Stream -- Summary -- Problems -- References -- Hypersonic Flows -- The Five Distinguishing Characteristics -- Newtonian Flow Model -- Stagnation Region Flow-Field Properties -- Modified Newtonian Flow -- High L/D Hypersonic Configurations-Waveriders -- Aerodynamic Heating -- A Hypersonic Cruiser for the Twenty-First Century? -- Importance of Interrelating CFD, Ground-Test Data, and Flight-Test Data -- Boundary-Layer-Transition Methodology -- Summary -- Problems -- References -- Aerodynamic Design Considerations -- High-Lift Configurations -- Circulation Control Wing -- Design Considerations for Tactical Military Aircraft -- Drag Reduction -- Development of an Airframe Modification to Improve the Mission Effectiveness of an Existing Airplane -- Considerations for Wing/Canard, Wing/Tail, and Tailless Configurations -- Comments on the F-15 Design -- The Design of the F-22 -- The Design of the F-35 -- Summary -- Problems -- References -- Tools for Defining the Aerodynamic Environment -- Computational Tools -- Establishing the Credibility of CFD Simulations. Ground-Based Test Programs -- Flight-Test Programs -- Integration of Experimental and Computational Tools: The Aerodynamic Design Philosophy -- Summary -- References -- Appendix A The Equations of Motion Written in Conservation Form -- Appendix B A Collection of Often Used Tables -- Answers to Selected Problems -- Index -- Credits. |
Record Nr. | UNINA-9910151656103321 |
Bertin John J. <1938->
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Boston : , : Pearson, , [2014] | ||
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Lo trovi qui: Univ. Federico II | ||
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Aerodynamics of bodies of revolution / N. F. Krasnov ; edited and annotated by Deane N. Morris ; translated from the second Russian edition by Joy B. Gazley |
Autore | Krasnov, Nikolai F. |
Pubbl/distr/stampa | New York : American Elsevier Publishing Company, 1970 |
Descrizione fisica | XIX, 895 p. : ill. ; 26 cm |
Disciplina | 629.1323 |
Soggetto non controllato |
Aerodinamica supersonica
Aerodinamica ipersonica |
ISBN | 0-444-00076-3 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-990000249710403321 |
Krasnov, Nikolai F.
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New York : American Elsevier Publishing Company, 1970 | ||
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Lo trovi qui: Univ. Federico II | ||
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Aerodynamics of tandem wing aircraft : from dinosaurs to UAVs and supersonic planes / / Illia Kryvokhatko |
Autore | Kryvokhatko Illia |
Edizione | [1st ed. 2023.] |
Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2023] |
Descrizione fisica | 1 online resource (183 pages) |
Disciplina | 629.1323 |
Soggetto topico |
Aerodynamics
Airplanes - Wings |
ISBN |
9783031237775
9783031237768 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Chapter 1. Historical Review -- Chapter 2. Determination of Tandem Wing Aircraft Aerodynamic Characteristics -- Chapter 3. Effect of Geometric Parameters on Aerodynamic Characteristics -- Chapter 4. Recommendations Regarding Aerodynamic Design of Tandem Wing Aircraft. |
Record Nr. | UNINA-9910678252603321 |
Kryvokhatko Illia
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Cham, Switzerland : , : Springer, , [2023] | ||
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Lo trovi qui: Univ. Federico II | ||
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Aerodynamics of wings and bodies / Holt Ashley, Marten Landahl |
Autore | Ashley, Holt |
Pubbl/distr/stampa | Reading [MA] : Addison-Wesley Publishing Company, c1965 |
Descrizione fisica | VII, 279 p. : ill. ; 24 cm |
Disciplina | 629.1323 |
Altri autori (Persone) | Landahl, Mårten |
Soggetto non controllato | Aerodinamica |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-990008447570403321 |
Ashley, Holt
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Reading [MA] : Addison-Wesley Publishing Company, c1965 | ||
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Lo trovi qui: Univ. Federico II | ||
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Aerodynamics, aeronautics and flight mechanics / B. W. McCormick |
Autore | McCormick, B. W., Barnes Warnock |
Edizione | [2. ed] |
Pubbl/distr/stampa | New York ; Chichester, : Wiley, 1995 |
Descrizione fisica | XII, 652 p. : ill. ; 26 cm. |
Disciplina | 629.1323 |
ISBN | 04-7111-087-6 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNICAMPANIA-SUN0035374 |
McCormick, B. W., Barnes Warnock
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New York ; Chichester, : Wiley, 1995 | ||
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Lo trovi qui: Univ. Vanvitelli | ||
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Aerodynamics, aeronautics and flight mechanics / Barnes W. McCormick |
Autore | MCCORMICK, Barnes W. |
Edizione | [2. ed.] |
Pubbl/distr/stampa | New York, : Wiley, 1995 |
Descrizione fisica | XII, 652 p. : ill. ; 26 cm |
Disciplina | 629.1323 |
Soggetto topico |
Aeroplani
Aerodinamica |
ISBN |
0-471-57506-2
9780471030324 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | und |
Record Nr. | UNISA-996434750403316 |
MCCORMICK, Barnes W.
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New York, : Wiley, 1995 | ||
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Lo trovi qui: Univ. di Salerno | ||
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