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Aircraft wake turbulence and its detection : proceedings of a symposium on aircraft wake turbulence held in Seattle, Washington, September 1-3, 1970, sponsored jointly by the Flight Sciences Laboratory, Boeing Scientific Research Laboratories and the Air Force Office of Scientific Research. / / edited by John H Olsen, Arnold Goldburg, Milton Rogers
| Aircraft wake turbulence and its detection : proceedings of a symposium on aircraft wake turbulence held in Seattle, Washington, September 1-3, 1970, sponsored jointly by the Flight Sciences Laboratory, Boeing Scientific Research Laboratories and the Air Force Office of Scientific Research. / / edited by John H Olsen, Arnold Goldburg, Milton Rogers |
| Edizione | [1st ed. 1971.] |
| Pubbl/distr/stampa | New York, New York ; ; London : , : Plenum Press, , [1971] |
| Descrizione fisica | 1 online resource (598 p.) |
| Disciplina | 629.13232 |
| Collana | Advisory circular |
| Soggetto topico | Wakes (Aerodynamics) |
| ISBN | 1-4684-8346-3 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Keynote Address -- Aircraft Wakes: A New Look at a Classical Problem -- Fundamental Problems -- The Velocity of Viscous Vortex Rings -- Studies in the Motion and Decay of Vortices -- Transport of a Vortex Wake in a Stably Stratified Atmosphere -- Experimental Methods -- Split-Film Anemometer Sensors for Three-Dimensional Velocity-Vector Measurement -- Sub-Scale Modeling of Aircraft Trailing Vortices -- The Utility of Doppler Radar in the Study of Aircraft Wing-Tip Vortices -- Application of Laser Doppler Systems to Vortex Measurement and Detection -- Wake Formation and Character -- An Analysis of Flight Measurements in the Wake of a Jet Transport Aircraft -- Vortex Control -- The Effect of a Drooped Wing Tip on Its Trailing Vortex System -- Some Work at the Royal Aircraft Establishment on the Behaviour of Vortex Wakes -- Span Loading and Formation of Wake -- An Experimental Investigation of Trailing Vortices Behind a Wing with a Vortex Dissipator -- Vortex Wake Development and Aircraft Dynamics -- Measurements of Boeing 747, Lockheed C5A and Other Aircraft Vortex Wake Characteristics by Tower Fly-by Technique -- Flight Evaluation of the Wing Vortex Wake Generated by Large Jet Transports -- Stability and Decay -- An Assessment of Dominant Mechanisms in Vortex-Wake Decay -- Theoretical and Experimental Study of the Stability of a Vortex Pair -- Structure of a Line Vortex in an Imposed Strain -- A New Look at the Dynamics of Vortices with Finite Cores -- Decay of an Isolated Vortex -- Decay of a Vortex Pair Behind an Aircraft -- Results of Trailing Vortex Studies in a Towing Tank -- Interactions with Vortex Wakes -- Results of the Boeing Company Wake Turbulence Test Program -- Aircraft Response to Turbulence Including Wakes -- Airloads and Moments on an Aircraft Flying Over a Pair of Inclined Trailing Vortices -- Aircraft Wake Turbulence Controllability Experiment -- Fog Formation and Dispersal by Trailing Vortices -- An Estimate of the Power Required to Eliminate Trailing Vortices by Suction -- Panel Discussion -- Conclusions -- Author Index. |
| Record Nr. | UNINA-9910698683603321 |
| New York, New York ; ; London : , : Plenum Press, , [1971] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Dynamics of compressible fluids : a textbook / / Oleksandr Girin
| Dynamics of compressible fluids : a textbook / / Oleksandr Girin |
| Autore | Girin Oleksandr |
| Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2022] |
| Descrizione fisica | 1 online resource (316 pages) |
| Disciplina | 629.13232 |
| Soggetto topico |
Compressibility
Fluid dynamics Shock waves |
| ISBN |
9783031112621
9783031112614 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Intro -- Preface -- Contents -- About the Author -- Introduction -- 1. Scope of the Dynamics of Compressible Fluids -- 2. The Subject Matter of Dynamics of Compressible Fluids -- 1 General Equations of Gas Motion -- 1.1 The Thermodynamic Model of a Perfect Gas -- Adiabatic Formulae -- 1.1.1 Internal State of a Gas Particle -- Thermodynamic Variables -- 1.1.2 Perfect Gas Model -- Polytropic Gas -- 1.1.3 Adiabatic Formulae -- 1.2 Governing Equations of Gas Motion -- Mathematical Model … -- 1.3 Speed of Propagation of Small Disturbances in Ideal Gas -- Sound Speed -- 1.4 Thermodynamics of a Moving Gas -- 1.4.1 Bernoulli-Saint-Venant Equation -- Enthalpy -- 1.4.2 Stagnation Gas State -- Isentropic Formulae -- 1.4.3 Laval's Number -- Other Characteristic States of a Moving Gas -- References -- 2 Continuous Flows -- 2.1 Equations of One-Dimensional Steady Gas Flow -- Rule of a Stream Reversal -- 2.2 Gas Outflow from Reservoir -- Saint-Venant-Vantzel Formula -- 2.3 Supersonic Outflow Mode -- Laval's Nozzle -- References -- 3 Discontinuity in a Gas Flow -- 3.1 Conservation Laws at a Strong Discontinuity Surface -- 3.2 Classification of Strong Discontinuities -- Shocks -- 3.3 Normal Shock Theory -- 3.4 Normal Shock Regularities -- 3.4.1 Velocity Jump -- 3.4.2 Pressure Jump -- 3.4.3 Density Jump -- 3.4.4 Entropy Jump -- 3.5 Shock Adiabatic Curve and Its Properties -- 3.5.1 Equation of Shock Adiabatic Curve -- 3.5.2 ``Asterisk'' Property -- 3.5.3 Limiting Degree of Gas Compression in Shock Waves -- 3.5.4 Approximation of Strong Shocks -- 3.5.5 Approximation of Weak Shocks -- References -- 4 Governing Equations and Initial-Boundary-Value Problems -- 4.1 Geometry of One-Dimensional Flows -- 4.2 Equations of Motion in Euler's Form -- Initial and Boundary Conditions -- 4.2.1 Euler's Equations of Motion -- 4.2.2 Initial Conditions -- 4.2.3 Boundary Conditions.
4.3 Equations of Motion in Lagrange's Form -- 4.4 Equations of Motion in Characteristic Form -- the Characteristic … -- 4.5 The Method of Characteristics -- 4.6 Generalized Cauchy Problem (Type I Problem) … -- 4.7 The Goursat Problem (Type II Problem) -- 4.8 Combined Problem of a Special Type (Type III Problem) -- 4.9 Characteristics as Trajectories of a Possible Weak Discontinuity of a Solution -- 4.9.1 Relationships Along the Weak Discontinuity Trajectory -- 4.9.2 Breakup of Arbitrary Weak Discontinuity -- References -- 5 Isentropic Gas Flows with Plane Waves -- 5.1 Riemann Method -- 5.1.1 Riemann Invariants -- 5.1.2 Riemann Variables -- Riemann Method -- 5.1.3 The Euler-Poisson Equation -- 5.1.4 The Remarkable Case γ= 3 -- 5.2 The Riemann Waves -- 5.2.1 Simple Waves -- 5.2.2 Adjoining Theorem -- 5.2.3 Simple Wave Equations -- 5.2.4 Properties of Simple Waves -- 5.3 Gradient Catastrophe -- 5.4 The Piston Problem -- 5.4.1 Case When the Piston Is Pulled Out from Gas -- 5.4.2 Case of Piston Moving with Constant Velocity -- 5.4.3 Gas Outflow into the Vacuum -- 5.4.4 Piston Moves into Gas -- Shock Wave Induction Time -- 5.5 Interaction of Simple Wave with a Contact Surface … -- 5.5.1 Analysis of the Flow Structure -- 5.5.2 Qualitative Analysis of the Interaction -- 5.5.3 The Limit Cases -- References -- 6 Methods of Wave Interaction Analysis -- 6.1 Method of (u, p)-Diagrams -- 6.1.1 ( u,p ) -Diagrams of Simple Waves -- 6.1.2 ( u,p ) -Diagrams of Shock Waves -- 6.2 Breakup of Arbitrary Strong Discontinuity (Riemann's Problem) -- 6.2.1 The Problem Formulation -- 6.2.2 Lemma About the Disturbances -- 6.2.3 Existence and Uniqueness of the Solution -- 6.2.4 Acoustic Approximation -- References -- 7 Shock-Wave Flows -- 7.1 Shock Tube Performance -- 7.1.1 The Device Description -- 7.1.2 The Problem Formulation -- 7.1.3 Shock Tube Solution. 7.2 Piston Moving with a Constant Velocity -- 7.2.1 Piston Moves into the Gas -- 7.2.2 Piston Moves Out from the Gas -- 7.3 Shock Wave Reflection from Rigid Wall -- Amplification Factor -- 7.3.1 The Problem Formulation -- 7.3.2 The Problem Solution -- 7.3.3 Shock Wave Percussive Ability -- 7.4 Interaction of Shock Wave with Contact Surface -- 7.4.1 The Problem Formulation -- 7.4.2 Qualitative Analysis of the Flow -- 7.5 Interaction of Two Shock Waves -- 7.5.1 The Problem Formulation -- 7.5.2 Qualitative Analysis -- 7.6 Interaction of Shock Wave with Simple Wave -- Entropy Trace -- 7.6.1 The Problem Formulation -- 7.6.2 Qualitative Analysis of the Flow -- 7.7 The Problem of the Internal Ballistics (Lagrange's Problem) -- 7.7.1 The Main Assumptions -- 7.7.2 The Problem Formulation -- 7.7.3 Solution in the Domain of Simple Wave -- 7.8 Strong Point Blast in Gas -- 7.8.1 Explosion Phenomenon -- 7.8.2 The Problem Formulation -- 7.8.3 Self-similarity of the Solution -- 7.8.4 Regularities of Gas Motion at Strong Point Blast -- 7.9 Long-Range Asymptotic Behavior of Shock Waves -- References -- 8 Steady Plane Irrotational Flows -- 8.1 Theory of an Oblique Shock -- 8.1.1 Interaction of Supersonic Flow with a Wedge -- Velocity Triangle -- 8.1.2 The Properties of Shock Polar -- 8.1.3 Oblique Reflection of a Plane Shock from a Rigid Wall -- 8.2 Equations of Steady Plane Irrotational Gas Motion -- 8.2.1 Equations and Methods -- 8.2.2 The Characteristics of Equations of Plane Irrotational Steady Flow -- 8.2.3 Simple Waves -- 8.3 Supersonic Flow Around a Convex Corner -- Prandtl-Meyer Flow -- 8.4 Plane Supersonic Outflow from a Slit -- 8.5 Elements of the Theory of Thin Aerodynamic Profile -- 8.5.1 The Main Concepts -- 8.5.2 Linearization of Equations of Motion -- 8.5.3 Thin Profile in a Subsonic Stream -- The Prandtl-Glauert Rule. 8.5.4 Thin Profile in a Supersonic Stream -- Akkeret's Formula -- Wave Drag -- References -- Appendix A Numerical Method of Characteristics for the 1-D Unsteady Flows (Massau's Scheme) -- A.1 General Features of the Method -- A.2 Algorithms of the Numerical Method of Characteristics -- A.2.1 Governing Equations of 1-D Unsteady Gas Flow in Characteristic Form -- A.2.2 Calculations in the Internal Node -- A.2.3 Implementation of Boundary Conditions -- A.2.3.1 ``Rigid Wall'' -- A.2.3.2 ``Piston'' -- A.2.3.3 ``Shock Front'' -- A.2.3.4 ``Contact Surface'' -- A.3 Reverse Method of Characteristics (Hartree Scheme) -- A.4 Scheme for Isentropic Flows with Plane Waves -- Appendix B Godunov's Method for the Calculations of 1-D Unsteady Flows -- B.1 General Properties of the Method -- B.2 Scheme of the Method -- B.2.1 Initial Data Processing -- B.2.2 Development of the Difference Scheme -- B.2.3 Searching for uk ,pk and Flow Configuration -- B.2.4 Determination of R,U,P -- B.2.5 Determination of the Slopes Wleft ,W'left ,Wk , W'right ,Wright of the Sectors' Borders -- B.2.6 Finding the Relevant Sector -- B.3 Approximate Solution of the Discontinuity Breakup Problem -- B.3.1 The Acoustic Approximation -- B.3.2 Isentropic Approximation -- B.4 Algorithms of Boundary Conditions' Fulfillment -- B.4.1 ``Rigid Wall'' -- B.4.2 ``Piston'' -- B.4.3 ``Shock Front'' -- B.4.4 ``Contact Surface'' -- B.5 Determination of a Stable Time-Step -- B.6 Example Structure and Flowchart of Program Code for Godunov's Method -- Appendix C Numerical Methods for Two-Dimensional Flows -- C.1 Method of Characteristics for 2-D Steady Supersonic Flows -- C.1.1 The Characteristic form of Equations of Gas Motion in Ehlers' Variables -- C.1.2 Calculation Scheme for an Internal Node -- C.1.3 Calculation Scheme at the Symmetry Axis. C.1.4 Calculation of the Node at the Rigid Wall -- C.1.5 Calculation of a Node at Free Surface -- C.2 Breakup-Based Scheme of the Predictor-Corrector Type for 2-D Steady Supersonic Flows -- C.2.1 Governing Equations -- C.2.2 Approximation of the Computational Domain -- C.2.3 The Corrector Stage: the Finite-Difference Scheme -- C.2.4 The Predictor Stage: Determination of R,U,V,P -- C.2.5 Boundary Condition Fulfillment -- C.2.6 Choice of Time Step -- Use of Auxiliary Variables -- C.3 Godunov's Scheme for 2-D Unsteady Flows -- C.3.1 The Case of Plane-Parallel Flow -- C.3.1.1 The ``Corrector'' Stage -- C.3.1.2 The Stage ``Predictor'' -- C.3.2 The Case of a Fixed Rectangular Grid -- References -- Index. |
| Record Nr. | UNINA-9910629298803321 |
Girin Oleksandr
|
||
| Cham, Switzerland : , : Springer, , [2022] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Dynamics of compressible fluids : a textbook / / Oleksandr Girin
| Dynamics of compressible fluids : a textbook / / Oleksandr Girin |
| Autore | Girin Oleksandr |
| Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2022] |
| Descrizione fisica | 1 online resource (316 pages) |
| Disciplina | 629.13232 |
| Soggetto topico |
Compressibility
Fluid dynamics Shock waves |
| ISBN |
9783031112621
9783031112614 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Intro -- Preface -- Contents -- About the Author -- Introduction -- 1. Scope of the Dynamics of Compressible Fluids -- 2. The Subject Matter of Dynamics of Compressible Fluids -- 1 General Equations of Gas Motion -- 1.1 The Thermodynamic Model of a Perfect Gas -- Adiabatic Formulae -- 1.1.1 Internal State of a Gas Particle -- Thermodynamic Variables -- 1.1.2 Perfect Gas Model -- Polytropic Gas -- 1.1.3 Adiabatic Formulae -- 1.2 Governing Equations of Gas Motion -- Mathematical Model … -- 1.3 Speed of Propagation of Small Disturbances in Ideal Gas -- Sound Speed -- 1.4 Thermodynamics of a Moving Gas -- 1.4.1 Bernoulli-Saint-Venant Equation -- Enthalpy -- 1.4.2 Stagnation Gas State -- Isentropic Formulae -- 1.4.3 Laval's Number -- Other Characteristic States of a Moving Gas -- References -- 2 Continuous Flows -- 2.1 Equations of One-Dimensional Steady Gas Flow -- Rule of a Stream Reversal -- 2.2 Gas Outflow from Reservoir -- Saint-Venant-Vantzel Formula -- 2.3 Supersonic Outflow Mode -- Laval's Nozzle -- References -- 3 Discontinuity in a Gas Flow -- 3.1 Conservation Laws at a Strong Discontinuity Surface -- 3.2 Classification of Strong Discontinuities -- Shocks -- 3.3 Normal Shock Theory -- 3.4 Normal Shock Regularities -- 3.4.1 Velocity Jump -- 3.4.2 Pressure Jump -- 3.4.3 Density Jump -- 3.4.4 Entropy Jump -- 3.5 Shock Adiabatic Curve and Its Properties -- 3.5.1 Equation of Shock Adiabatic Curve -- 3.5.2 ``Asterisk'' Property -- 3.5.3 Limiting Degree of Gas Compression in Shock Waves -- 3.5.4 Approximation of Strong Shocks -- 3.5.5 Approximation of Weak Shocks -- References -- 4 Governing Equations and Initial-Boundary-Value Problems -- 4.1 Geometry of One-Dimensional Flows -- 4.2 Equations of Motion in Euler's Form -- Initial and Boundary Conditions -- 4.2.1 Euler's Equations of Motion -- 4.2.2 Initial Conditions -- 4.2.3 Boundary Conditions.
4.3 Equations of Motion in Lagrange's Form -- 4.4 Equations of Motion in Characteristic Form -- the Characteristic … -- 4.5 The Method of Characteristics -- 4.6 Generalized Cauchy Problem (Type I Problem) … -- 4.7 The Goursat Problem (Type II Problem) -- 4.8 Combined Problem of a Special Type (Type III Problem) -- 4.9 Characteristics as Trajectories of a Possible Weak Discontinuity of a Solution -- 4.9.1 Relationships Along the Weak Discontinuity Trajectory -- 4.9.2 Breakup of Arbitrary Weak Discontinuity -- References -- 5 Isentropic Gas Flows with Plane Waves -- 5.1 Riemann Method -- 5.1.1 Riemann Invariants -- 5.1.2 Riemann Variables -- Riemann Method -- 5.1.3 The Euler-Poisson Equation -- 5.1.4 The Remarkable Case γ= 3 -- 5.2 The Riemann Waves -- 5.2.1 Simple Waves -- 5.2.2 Adjoining Theorem -- 5.2.3 Simple Wave Equations -- 5.2.4 Properties of Simple Waves -- 5.3 Gradient Catastrophe -- 5.4 The Piston Problem -- 5.4.1 Case When the Piston Is Pulled Out from Gas -- 5.4.2 Case of Piston Moving with Constant Velocity -- 5.4.3 Gas Outflow into the Vacuum -- 5.4.4 Piston Moves into Gas -- Shock Wave Induction Time -- 5.5 Interaction of Simple Wave with a Contact Surface … -- 5.5.1 Analysis of the Flow Structure -- 5.5.2 Qualitative Analysis of the Interaction -- 5.5.3 The Limit Cases -- References -- 6 Methods of Wave Interaction Analysis -- 6.1 Method of (u, p)-Diagrams -- 6.1.1 ( u,p ) -Diagrams of Simple Waves -- 6.1.2 ( u,p ) -Diagrams of Shock Waves -- 6.2 Breakup of Arbitrary Strong Discontinuity (Riemann's Problem) -- 6.2.1 The Problem Formulation -- 6.2.2 Lemma About the Disturbances -- 6.2.3 Existence and Uniqueness of the Solution -- 6.2.4 Acoustic Approximation -- References -- 7 Shock-Wave Flows -- 7.1 Shock Tube Performance -- 7.1.1 The Device Description -- 7.1.2 The Problem Formulation -- 7.1.3 Shock Tube Solution. 7.2 Piston Moving with a Constant Velocity -- 7.2.1 Piston Moves into the Gas -- 7.2.2 Piston Moves Out from the Gas -- 7.3 Shock Wave Reflection from Rigid Wall -- Amplification Factor -- 7.3.1 The Problem Formulation -- 7.3.2 The Problem Solution -- 7.3.3 Shock Wave Percussive Ability -- 7.4 Interaction of Shock Wave with Contact Surface -- 7.4.1 The Problem Formulation -- 7.4.2 Qualitative Analysis of the Flow -- 7.5 Interaction of Two Shock Waves -- 7.5.1 The Problem Formulation -- 7.5.2 Qualitative Analysis -- 7.6 Interaction of Shock Wave with Simple Wave -- Entropy Trace -- 7.6.1 The Problem Formulation -- 7.6.2 Qualitative Analysis of the Flow -- 7.7 The Problem of the Internal Ballistics (Lagrange's Problem) -- 7.7.1 The Main Assumptions -- 7.7.2 The Problem Formulation -- 7.7.3 Solution in the Domain of Simple Wave -- 7.8 Strong Point Blast in Gas -- 7.8.1 Explosion Phenomenon -- 7.8.2 The Problem Formulation -- 7.8.3 Self-similarity of the Solution -- 7.8.4 Regularities of Gas Motion at Strong Point Blast -- 7.9 Long-Range Asymptotic Behavior of Shock Waves -- References -- 8 Steady Plane Irrotational Flows -- 8.1 Theory of an Oblique Shock -- 8.1.1 Interaction of Supersonic Flow with a Wedge -- Velocity Triangle -- 8.1.2 The Properties of Shock Polar -- 8.1.3 Oblique Reflection of a Plane Shock from a Rigid Wall -- 8.2 Equations of Steady Plane Irrotational Gas Motion -- 8.2.1 Equations and Methods -- 8.2.2 The Characteristics of Equations of Plane Irrotational Steady Flow -- 8.2.3 Simple Waves -- 8.3 Supersonic Flow Around a Convex Corner -- Prandtl-Meyer Flow -- 8.4 Plane Supersonic Outflow from a Slit -- 8.5 Elements of the Theory of Thin Aerodynamic Profile -- 8.5.1 The Main Concepts -- 8.5.2 Linearization of Equations of Motion -- 8.5.3 Thin Profile in a Subsonic Stream -- The Prandtl-Glauert Rule. 8.5.4 Thin Profile in a Supersonic Stream -- Akkeret's Formula -- Wave Drag -- References -- Appendix A Numerical Method of Characteristics for the 1-D Unsteady Flows (Massau's Scheme) -- A.1 General Features of the Method -- A.2 Algorithms of the Numerical Method of Characteristics -- A.2.1 Governing Equations of 1-D Unsteady Gas Flow in Characteristic Form -- A.2.2 Calculations in the Internal Node -- A.2.3 Implementation of Boundary Conditions -- A.2.3.1 ``Rigid Wall'' -- A.2.3.2 ``Piston'' -- A.2.3.3 ``Shock Front'' -- A.2.3.4 ``Contact Surface'' -- A.3 Reverse Method of Characteristics (Hartree Scheme) -- A.4 Scheme for Isentropic Flows with Plane Waves -- Appendix B Godunov's Method for the Calculations of 1-D Unsteady Flows -- B.1 General Properties of the Method -- B.2 Scheme of the Method -- B.2.1 Initial Data Processing -- B.2.2 Development of the Difference Scheme -- B.2.3 Searching for uk ,pk and Flow Configuration -- B.2.4 Determination of R,U,P -- B.2.5 Determination of the Slopes Wleft ,W'left ,Wk , W'right ,Wright of the Sectors' Borders -- B.2.6 Finding the Relevant Sector -- B.3 Approximate Solution of the Discontinuity Breakup Problem -- B.3.1 The Acoustic Approximation -- B.3.2 Isentropic Approximation -- B.4 Algorithms of Boundary Conditions' Fulfillment -- B.4.1 ``Rigid Wall'' -- B.4.2 ``Piston'' -- B.4.3 ``Shock Front'' -- B.4.4 ``Contact Surface'' -- B.5 Determination of a Stable Time-Step -- B.6 Example Structure and Flowchart of Program Code for Godunov's Method -- Appendix C Numerical Methods for Two-Dimensional Flows -- C.1 Method of Characteristics for 2-D Steady Supersonic Flows -- C.1.1 The Characteristic form of Equations of Gas Motion in Ehlers' Variables -- C.1.2 Calculation Scheme for an Internal Node -- C.1.3 Calculation Scheme at the Symmetry Axis. C.1.4 Calculation of the Node at the Rigid Wall -- C.1.5 Calculation of a Node at Free Surface -- C.2 Breakup-Based Scheme of the Predictor-Corrector Type for 2-D Steady Supersonic Flows -- C.2.1 Governing Equations -- C.2.2 Approximation of the Computational Domain -- C.2.3 The Corrector Stage: the Finite-Difference Scheme -- C.2.4 The Predictor Stage: Determination of R,U,V,P -- C.2.5 Boundary Condition Fulfillment -- C.2.6 Choice of Time Step -- Use of Auxiliary Variables -- C.3 Godunov's Scheme for 2-D Unsteady Flows -- C.3.1 The Case of Plane-Parallel Flow -- C.3.1.1 The ``Corrector'' Stage -- C.3.1.2 The Stage ``Predictor'' -- C.3.2 The Case of a Fixed Rectangular Grid -- References -- Index. |
| Record Nr. | UNISA-996499863703316 |
|
Girin Oleksandr
|
||
| Cham, Switzerland : , : Springer, , [2022] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. di Salerno | ||
| ||
Hypersonic flow research [[electronic resource] ] : a selection of technical papers based mainly on a symposium of the American Rocket Society held at Massachusetts Institute of Technology / / edited by Frederick R. Riddell
| Hypersonic flow research [[electronic resource] ] : a selection of technical papers based mainly on a symposium of the American Rocket Society held at Massachusetts Institute of Technology / / edited by Frederick R. Riddell |
| Pubbl/distr/stampa | New York, : Academic Press, 1962 |
| Descrizione fisica | 1 online resource (768 p.) |
| Disciplina | 629.13232 |
| Altri autori (Persone) | RiddellFrederick R |
| Collana | Progress in astronautics and rocketry |
| Soggetto topico | Aerodynamics, Hypersonic |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-481-3
1-60086-262-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Hypersonics Committee""; ""Preface""; ""Contents""; ""The ARS � AFOSR International Hypersonics Conference: Summary and Comments""; ""A. Hypersonic Flow at Low Reynolds Number""; ""Introduction""; ""Density Behavior along the Stagnation Line of a Blunt Body in Hyperthermal Flow""; ""Second-Order Compressible Boundary Layer Theory with Application to Blunt Bodies in Hypersonic Flow""; ""Comment on above paper""; ""Rarefied Hypersonic Flow over a Sphere""; ""The Rayleigh Problem for a Dissociated Gas""; ""B. Chemical Kinetic Effects in Hypersonic Flow""
""Introduction""""Chemical Kinetics: A General Introduction""; ""Chemical Kinetics of High Temperature Air""; ""Chemical Effects in External Hypersonic Flows""; ""Radiation at Hypersonic Speeds""; ""Radiation from the Nonequilibrium Shock Front""; ""C. Inviscid Hypersonic Flow""; ""Introduction""; ""Slender Wings at High Angles of Attack in Hypersonic Flows""; ""Newtonian Theory of Hypersonic Flow at Large Distances from Bluff Axially Symmetric Bodies""; ""Shock Layer Structure and Entropy Layers in Hypersonic Conical Flows""; ""Theory of Entropy Layers and Nose Bluntness in Hypersonic Flow"" ""D. Experimental Techniques I""""Introduction""; ""Aerodynamic Testing at Mach Numbers from 15 to 20""; ""The Duration and Properties of the Flow in a Hypersonic Shock Tunnel""; ""An Evaluation of the Hypersonic Gun Tunnel""; ""Diagnostic Studies of a Low Density, Arc Heated Wind Tunnel Stream""; ""Initial Results from a Low Density, Hypervelocity Wind Tunnel""; ""E. Experimental Techniques II""; ""Introduction""; ""The Free Flight Range: A Tool for Research in the Physics of High Speed Flight""; ""Survey of Shock Tube Research Related to the Aerophysics Problem of Hypersonic Flight"" ""Air Arc Simulation of Hypersonic Environments""""Development of the Shock Tunnel and Its Application to Hypersonic Flight"" |
| Record Nr. | UNINA-9910456961803321 |
| New York, : Academic Press, 1962 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hypersonic flow research [[electronic resource] ] : a selection of technical papers based mainly on a symposium of the American Rocket Society held at Massachusetts Institute of Technology / / edited by Frederick R. Riddell
| Hypersonic flow research [[electronic resource] ] : a selection of technical papers based mainly on a symposium of the American Rocket Society held at Massachusetts Institute of Technology / / edited by Frederick R. Riddell |
| Pubbl/distr/stampa | New York, : Academic Press, 1962 |
| Descrizione fisica | 1 online resource (768 p.) |
| Disciplina | 629.13232 |
| Altri autori (Persone) | RiddellFrederick R |
| Collana | Progress in astronautics and rocketry |
| Soggetto topico | Aerodynamics, Hypersonic |
| ISBN |
1-60086-481-3
1-60086-262-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Hypersonics Committee""; ""Preface""; ""Contents""; ""The ARS � AFOSR International Hypersonics Conference: Summary and Comments""; ""A. Hypersonic Flow at Low Reynolds Number""; ""Introduction""; ""Density Behavior along the Stagnation Line of a Blunt Body in Hyperthermal Flow""; ""Second-Order Compressible Boundary Layer Theory with Application to Blunt Bodies in Hypersonic Flow""; ""Comment on above paper""; ""Rarefied Hypersonic Flow over a Sphere""; ""The Rayleigh Problem for a Dissociated Gas""; ""B. Chemical Kinetic Effects in Hypersonic Flow""
""Introduction""""Chemical Kinetics: A General Introduction""; ""Chemical Kinetics of High Temperature Air""; ""Chemical Effects in External Hypersonic Flows""; ""Radiation at Hypersonic Speeds""; ""Radiation from the Nonequilibrium Shock Front""; ""C. Inviscid Hypersonic Flow""; ""Introduction""; ""Slender Wings at High Angles of Attack in Hypersonic Flows""; ""Newtonian Theory of Hypersonic Flow at Large Distances from Bluff Axially Symmetric Bodies""; ""Shock Layer Structure and Entropy Layers in Hypersonic Conical Flows""; ""Theory of Entropy Layers and Nose Bluntness in Hypersonic Flow"" ""D. Experimental Techniques I""""Introduction""; ""Aerodynamic Testing at Mach Numbers from 15 to 20""; ""The Duration and Properties of the Flow in a Hypersonic Shock Tunnel""; ""An Evaluation of the Hypersonic Gun Tunnel""; ""Diagnostic Studies of a Low Density, Arc Heated Wind Tunnel Stream""; ""Initial Results from a Low Density, Hypervelocity Wind Tunnel""; ""E. Experimental Techniques II""; ""Introduction""; ""The Free Flight Range: A Tool for Research in the Physics of High Speed Flight""; ""Survey of Shock Tube Research Related to the Aerophysics Problem of Hypersonic Flight"" ""Air Arc Simulation of Hypersonic Environments""""Development of the Shock Tunnel and Its Application to Hypersonic Flight"" |
| Record Nr. | UNINA-9910781414703321 |
| New York, : Academic Press, 1962 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hypersonic flow research [[electronic resource] ] : a selection of technical papers based mainly on a symposium of the American Rocket Society held at Massachusetts Institute of Technology / / edited by Frederick R. Riddell
| Hypersonic flow research [[electronic resource] ] : a selection of technical papers based mainly on a symposium of the American Rocket Society held at Massachusetts Institute of Technology / / edited by Frederick R. Riddell |
| Pubbl/distr/stampa | New York, : Academic Press, 1962 |
| Descrizione fisica | 1 online resource (768 p.) |
| Disciplina | 629.13232 |
| Altri autori (Persone) | RiddellFrederick R |
| Collana | Progress in astronautics and rocketry |
| Soggetto topico | Aerodynamics, Hypersonic |
| ISBN |
1-60086-481-3
1-60086-262-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Hypersonics Committee""; ""Preface""; ""Contents""; ""The ARS � AFOSR International Hypersonics Conference: Summary and Comments""; ""A. Hypersonic Flow at Low Reynolds Number""; ""Introduction""; ""Density Behavior along the Stagnation Line of a Blunt Body in Hyperthermal Flow""; ""Second-Order Compressible Boundary Layer Theory with Application to Blunt Bodies in Hypersonic Flow""; ""Comment on above paper""; ""Rarefied Hypersonic Flow over a Sphere""; ""The Rayleigh Problem for a Dissociated Gas""; ""B. Chemical Kinetic Effects in Hypersonic Flow""
""Introduction""""Chemical Kinetics: A General Introduction""; ""Chemical Kinetics of High Temperature Air""; ""Chemical Effects in External Hypersonic Flows""; ""Radiation at Hypersonic Speeds""; ""Radiation from the Nonequilibrium Shock Front""; ""C. Inviscid Hypersonic Flow""; ""Introduction""; ""Slender Wings at High Angles of Attack in Hypersonic Flows""; ""Newtonian Theory of Hypersonic Flow at Large Distances from Bluff Axially Symmetric Bodies""; ""Shock Layer Structure and Entropy Layers in Hypersonic Conical Flows""; ""Theory of Entropy Layers and Nose Bluntness in Hypersonic Flow"" ""D. Experimental Techniques I""""Introduction""; ""Aerodynamic Testing at Mach Numbers from 15 to 20""; ""The Duration and Properties of the Flow in a Hypersonic Shock Tunnel""; ""An Evaluation of the Hypersonic Gun Tunnel""; ""Diagnostic Studies of a Low Density, Arc Heated Wind Tunnel Stream""; ""Initial Results from a Low Density, Hypervelocity Wind Tunnel""; ""E. Experimental Techniques II""; ""Introduction""; ""The Free Flight Range: A Tool for Research in the Physics of High Speed Flight""; ""Survey of Shock Tube Research Related to the Aerophysics Problem of Hypersonic Flight"" ""Air Arc Simulation of Hypersonic Environments""""Development of the Shock Tunnel and Its Application to Hypersonic Flight"" |
| Record Nr. | UNINA-9910826976203321 |
| New York, : Academic Press, 1962 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Secondary Instabilities of Görtler Vortices in High-Speed Boundary Layers : Mechanisms and Flow Control on Laminar-Turbulent Transition / / by Jie Ren
| Secondary Instabilities of Görtler Vortices in High-Speed Boundary Layers : Mechanisms and Flow Control on Laminar-Turbulent Transition / / by Jie Ren |
| Autore | Ren Jie |
| Edizione | [1st ed. 2018.] |
| Pubbl/distr/stampa | Singapore : , : Springer Singapore : , : Imprint : Springer, , 2018 |
| Descrizione fisica | 1 online resource (XVIII, 94 p. 51 illus., 41 illus. in color.) |
| Disciplina | 629.13232 |
| Collana | Springer Theses, Recognizing Outstanding Ph.D. Research |
| Soggetto topico |
Fluid mechanics
Mechanics Applied mathematics Engineering mathematics Engineering Fluid Dynamics Classical Mechanics Mathematical and Computational Engineering |
| ISBN | 981-10-6832-1 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910299561103321 |
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Ren Jie
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| Singapore : , : Springer Singapore : , : Imprint : Springer, , 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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