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Analysis of the stability of a thin liquid film adjacent to a high-speed gas stream / / by Philip R. Nachtsheim
| Analysis of the stability of a thin liquid film adjacent to a high-speed gas stream / / by Philip R. Nachtsheim |
| Autore | Nachtsheim Philip R. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 |
| Descrizione fisica | 1 online resource (33 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Fluid mechanics
Gas streams Atmospheric waves - Mathematical models Space vehicles - Atmospheric entry |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716075603321 |
Nachtsheim Philip R.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Dynamics of atmospheric re-entry [[electronic resource] /] / Frank J. Regan, Satya M. Anandakrishnan
| Dynamics of atmospheric re-entry [[electronic resource] /] / Frank J. Regan, Satya M. Anandakrishnan |
| Autore | Regan Frank J |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1993 |
| Descrizione fisica | 1 online resource (603 p.) |
| Disciplina | 629.4/15 |
| Altri autori (Persone) | AnandakrishnanSatya M |
| Collana | AIAA education series |
| Soggetto topico |
Space vehicles - Atmospheric entry
Space vehicles - Aerodynamics |
| Soggetto genere / forma | Electronic books. |
| ISBN | 1-60086-046-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Preface""; ""Table of Contents""; ""Chapter 1. Introduction""; ""1.0 Background""; ""1.1 Meteorites�Nature's (Re-)Entry Bodies""; ""1.2 Artifacts�Manmade Re-Entry Bodies""; ""1.3 Overview""; ""References""; ""Chapter 2. Atmospheric Model""; ""2.1 Introduction""; ""2.2 Standard Atmospheres""; ""2.3 Atmospheric Description""; ""2.4 Physical Foundations of an Atmospheric Model""; ""2.5 Derived Atmospheric Quantities""; ""2.6 Exponential Atmosphere""; ""2.7 Planetary Atmospheres""; ""References""
""Chapter 3. Earth's Form and Gravitational Field""""3.1 Introduction""; ""3.2 Geoid and Reference Ellipsoid""; ""3.3 Geocentric Position Vector""; ""3.4 Deflection of the Vertical""; ""3.5 Earth's Radius""; ""3.6 Earth's Gravitational Potential""; ""3.7 Gravitational Field in an Inertial Frame""; ""3.8 Gravitational Anomalies and Deflection of the Vertical""; ""3.9 Longitudinal Dependencies""; ""3.10 Gravity Gradient""; ""References""; ""Chapter 4. Axis Transformations""; ""4.1 Background""; ""4.2 Directional Cosine Matrix""; ""4.3 Updating the DCM""; ""4.4 Euler Angles"" ""4.5 Updating Euler Angles""""4.6 Axis/Angle Parameters""; ""4.7 Updating the Axis/Angle Parameters""; ""4.8 Euler Four-Parameter Method (Quaternions)""; ""4.9 Summary""; ""References""; ""Chapter 5. Force and Moment Equations""; ""5.1 Newton's Second Law of Motion""; ""5.2 Vector Differentiation""; ""5.3 Force Equations""; ""5.4 Moment Equations""; ""5.5 Calculation of the Moments and Products of Inertia""; ""References""; ""Bibliography""; ""Chapter 6. Keplerian Motion""; ""6.1 Equations of Motion""; ""6.2 Impact Equations""; ""6.3 Time of Flight""; ""6.4 Error Analysis"" ""6.5 Oblateness Effects""""6.6 Earth Rotation Effects""; ""6.7 Deployment Attitudes""; ""6.8 Summary""; ""References""; ""Chapter 7. Re-Entry Vehicle Particle Mechanics""; ""7.1 Re-Entry Physics""; ""7.2 Equations of Planar Motion""; ""7.3 Re-Entry Case Studies""; ""7.4 Some Nondimensional Representations""; ""7.5 Heat Transfer and Dynamics""; ""References""; ""Chapter 8. Decoys and the Identification of Re-Entry Vehicles""; ""8.1 Introduction""; ""8.2 Estimators""; ""8.3 Decoy Effectiveness""; ""References""; ""Chapter 9. Maneuvering Re-Entry Vehicles: Particle Motion"" ""9.1 Introduction""""9.2 Drag Polar""; ""9.3 MaRV State Equations""; ""9.4 Diveline Guidance""; ""9.5 Determining the Projected Interception Point""; ""9.6 Interceptor Guidance Equations""; ""9.7 Interceptor State Equations""; ""9.8 Simulation Results""; ""9.9 Other Guidance Laws and Summary""; ""References""; ""Bibliography""; ""Chapter 10. Angular Motion During the Exoatmospheric (Keplerian) Phase""; ""10.1 Introduction""; ""10.2 Re-Entry Vehicle Deployment""; ""10.3 Analytical Treatment of Torque-Free Motion""; ""10.4 Torque-Free Motion�Poinsot Construction""; ""10.5 Relative Motion"" ""References"" |
| Record Nr. | UNINA-9910457230503321 |
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Regan Frank J
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| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1993 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Dynamics of atmospheric re-entry [[electronic resource] /] / Frank J. Regan, Satya M. Anandakrishnan
| Dynamics of atmospheric re-entry [[electronic resource] /] / Frank J. Regan, Satya M. Anandakrishnan |
| Autore | Regan Frank J |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1993 |
| Descrizione fisica | 1 online resource (603 p.) |
| Disciplina | 629.4/15 |
| Altri autori (Persone) | AnandakrishnanSatya M |
| Collana | AIAA education series |
| Soggetto topico |
Space vehicles - Atmospheric entry
Space vehicles - Aerodynamics |
| ISBN | 1-60086-046-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Preface""; ""Table of Contents""; ""Chapter 1. Introduction""; ""1.0 Background""; ""1.1 Meteorites�Nature's (Re-)Entry Bodies""; ""1.2 Artifacts�Manmade Re-Entry Bodies""; ""1.3 Overview""; ""References""; ""Chapter 2. Atmospheric Model""; ""2.1 Introduction""; ""2.2 Standard Atmospheres""; ""2.3 Atmospheric Description""; ""2.4 Physical Foundations of an Atmospheric Model""; ""2.5 Derived Atmospheric Quantities""; ""2.6 Exponential Atmosphere""; ""2.7 Planetary Atmospheres""; ""References""
""Chapter 3. Earth's Form and Gravitational Field""""3.1 Introduction""; ""3.2 Geoid and Reference Ellipsoid""; ""3.3 Geocentric Position Vector""; ""3.4 Deflection of the Vertical""; ""3.5 Earth's Radius""; ""3.6 Earth's Gravitational Potential""; ""3.7 Gravitational Field in an Inertial Frame""; ""3.8 Gravitational Anomalies and Deflection of the Vertical""; ""3.9 Longitudinal Dependencies""; ""3.10 Gravity Gradient""; ""References""; ""Chapter 4. Axis Transformations""; ""4.1 Background""; ""4.2 Directional Cosine Matrix""; ""4.3 Updating the DCM""; ""4.4 Euler Angles"" ""4.5 Updating Euler Angles""""4.6 Axis/Angle Parameters""; ""4.7 Updating the Axis/Angle Parameters""; ""4.8 Euler Four-Parameter Method (Quaternions)""; ""4.9 Summary""; ""References""; ""Chapter 5. Force and Moment Equations""; ""5.1 Newton's Second Law of Motion""; ""5.2 Vector Differentiation""; ""5.3 Force Equations""; ""5.4 Moment Equations""; ""5.5 Calculation of the Moments and Products of Inertia""; ""References""; ""Bibliography""; ""Chapter 6. Keplerian Motion""; ""6.1 Equations of Motion""; ""6.2 Impact Equations""; ""6.3 Time of Flight""; ""6.4 Error Analysis"" ""6.5 Oblateness Effects""""6.6 Earth Rotation Effects""; ""6.7 Deployment Attitudes""; ""6.8 Summary""; ""References""; ""Chapter 7. Re-Entry Vehicle Particle Mechanics""; ""7.1 Re-Entry Physics""; ""7.2 Equations of Planar Motion""; ""7.3 Re-Entry Case Studies""; ""7.4 Some Nondimensional Representations""; ""7.5 Heat Transfer and Dynamics""; ""References""; ""Chapter 8. Decoys and the Identification of Re-Entry Vehicles""; ""8.1 Introduction""; ""8.2 Estimators""; ""8.3 Decoy Effectiveness""; ""References""; ""Chapter 9. Maneuvering Re-Entry Vehicles: Particle Motion"" ""9.1 Introduction""""9.2 Drag Polar""; ""9.3 MaRV State Equations""; ""9.4 Diveline Guidance""; ""9.5 Determining the Projected Interception Point""; ""9.6 Interceptor Guidance Equations""; ""9.7 Interceptor State Equations""; ""9.8 Simulation Results""; ""9.9 Other Guidance Laws and Summary""; ""References""; ""Bibliography""; ""Chapter 10. Angular Motion During the Exoatmospheric (Keplerian) Phase""; ""10.1 Introduction""; ""10.2 Re-Entry Vehicle Deployment""; ""10.3 Analytical Treatment of Torque-Free Motion""; ""10.4 Torque-Free Motion�Poinsot Construction""; ""10.5 Relative Motion"" ""References"" |
| Record Nr. | UNINA-9910781402503321 |
|
Regan Frank J
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| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1993 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration / / by Louis E. Clark
| Effect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration / / by Louis E. Clark |
| Autore | Clark Louis E. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , December 1972 |
| Descrizione fisica | 1 online resource (52 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerospace vehicles
Aerodynamics Space vehicles - Atmospheric entry Leading edges (Aerodynamics) Aerodynamic heating Aerothermodynamics Space shuttles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716019303321 |
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Clark Louis E.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , December 1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Entries from earth orbit that simulate acceleration stresses of manned planetary missions / / by Frederick G. Edwards
| Entries from earth orbit that simulate acceleration stresses of manned planetary missions / / by Frederick G. Edwards |
| Autore | Edwards Frederick G. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 |
| Descrizione fisica | 1 online resource (32 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Acceleration (Mechanics)
Interplanetary voyages Space vehicles - Atmospheric entry Weightlessness |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714070103321 |
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Edwards Frederick G.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Entry vehicle heating and thermal protection systems [[electronic resource] ] : Space Shuttle, Solar Starprobe, Jupiter Galileo Probe / / edited by Paul E. Bauer, Howard E. Collicott
| Entry vehicle heating and thermal protection systems [[electronic resource] ] : Space Shuttle, Solar Starprobe, Jupiter Galileo Probe / / edited by Paul E. Bauer, Howard E. Collicott |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, c1983 |
| Descrizione fisica | 1 online resource (588 p.) |
| Disciplina |
629.1 s
629.44/1 |
| Altri autori (Persone) |
BauerPaul E. <1924->
CollicottHoward E |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Space vehicles - Thermodynamics
Space vehicles - Atmospheric entry |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-562-3
1-60086-343-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Editorial Committee""; ""List of Series Volumes""; ""Chapter I. Space Shuttle Aeroheating""; ""Aerothermodynamic Entry Environment of the Space Shuttle Orbiter""; ""Approximate Method of Predicting Heating on the Windward Side of Space Shuttle Orbiter and Comparisons with Flight Data""; ""Viscous Shock-Layer Predictions for Hypersonic Laminar or Turbulent Flows in Chemical Equilibrium over the Windward Surface of a Shuttle-Like Vehicle""
""Influence of Radiant Energy Exchange on the Determination of Convective Heat-Transfer Rates to Orbiter Leeside Surfaces during Entry""""Catalytic Efficiency of the Space Shuttle Heat Shield""; ""Catalytic Recombination/Space Shuttle Heating""; ""Viscous Shock-Layer Heating Analysis for the Shuttle Windward Symmetry Plane with Surface Finite Catalytic Recombination Rates""; ""Chapter II. Space Shuttle Thermal Protection""; ""Shuttle Orbiter Reusable Surface Insulation Thermal Performance""; ""Space Shuttle Orbiter Leading Edge Thermal Performance"" ""Comparison of Orbiter STS-2 Development Flight Instrumentation Data with Thermal Math Model Predictions""""Flight Measurements of Tile Gap Heating on the Space Shuttle""; ""Tile-Gap Flow in the Shuttle Orbiter Thermal Protection System""; ""Assessment of Alternate Thermal Protection Systemsfor the Space Shuttle Orbiter""; ""Initial Shuttle External Tank Aerothermal Flight Evaluation""; ""Chapter III. Solar Starprobe Heat Shielding""; ""STARPROBE Thermal Shield System Design Concepts""; ""Preliminary Design of the Thermal Protection System for Solar Probe"" ""Chapter IV. Jupiter Galileo Probe Entry Heating and Protection""""Galileo Probe Forebody Flowfield Predictions""; ""An Evaluation of Turbulence Models for Massively Blown Surfaces""; ""Trajectories of Solid Particles Spalled from a Carbonaceous Heat Shield""; ""Spallation of the Galileo Probe Heat Shield""; ""Response of Galileo Aft Cover Componentsto Laser Radiation""; ""Author Index for Volume 85"" |
| Record Nr. | UNINA-9910457235603321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, c1983 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Entry vehicle heating and thermal protection systems [[electronic resource] ] : Space Shuttle, Solar Starprobe, Jupiter Galileo Probe / / edited by Paul E. Bauer, Howard E. Collicott
| Entry vehicle heating and thermal protection systems [[electronic resource] ] : Space Shuttle, Solar Starprobe, Jupiter Galileo Probe / / edited by Paul E. Bauer, Howard E. Collicott |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, c1983 |
| Descrizione fisica | 1 online resource (588 p.) |
| Disciplina |
629.1 s
629.44/1 |
| Altri autori (Persone) |
BauerPaul E. <1924->
CollicottHoward E |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Space vehicles - Thermodynamics
Space vehicles - Atmospheric entry |
| ISBN |
1-60086-562-3
1-60086-343-4 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Editorial Committee""; ""List of Series Volumes""; ""Chapter I. Space Shuttle Aeroheating""; ""Aerothermodynamic Entry Environment of the Space Shuttle Orbiter""; ""Approximate Method of Predicting Heating on the Windward Side of Space Shuttle Orbiter and Comparisons with Flight Data""; ""Viscous Shock-Layer Predictions for Hypersonic Laminar or Turbulent Flows in Chemical Equilibrium over the Windward Surface of a Shuttle-Like Vehicle""
""Influence of Radiant Energy Exchange on the Determination of Convective Heat-Transfer Rates to Orbiter Leeside Surfaces during Entry""""Catalytic Efficiency of the Space Shuttle Heat Shield""; ""Catalytic Recombination/Space Shuttle Heating""; ""Viscous Shock-Layer Heating Analysis for the Shuttle Windward Symmetry Plane with Surface Finite Catalytic Recombination Rates""; ""Chapter II. Space Shuttle Thermal Protection""; ""Shuttle Orbiter Reusable Surface Insulation Thermal Performance""; ""Space Shuttle Orbiter Leading Edge Thermal Performance"" ""Comparison of Orbiter STS-2 Development Flight Instrumentation Data with Thermal Math Model Predictions""""Flight Measurements of Tile Gap Heating on the Space Shuttle""; ""Tile-Gap Flow in the Shuttle Orbiter Thermal Protection System""; ""Assessment of Alternate Thermal Protection Systemsfor the Space Shuttle Orbiter""; ""Initial Shuttle External Tank Aerothermal Flight Evaluation""; ""Chapter III. Solar Starprobe Heat Shielding""; ""STARPROBE Thermal Shield System Design Concepts""; ""Preliminary Design of the Thermal Protection System for Solar Probe"" ""Chapter IV. Jupiter Galileo Probe Entry Heating and Protection""""Galileo Probe Forebody Flowfield Predictions""; ""An Evaluation of Turbulence Models for Massively Blown Surfaces""; ""Trajectories of Solid Particles Spalled from a Carbonaceous Heat Shield""; ""Spallation of the Galileo Probe Heat Shield""; ""Response of Galileo Aft Cover Componentsto Laser Radiation""; ""Author Index for Volume 85"" |
| Record Nr. | UNINA-9910781418003321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, c1983 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
A flight measurement of optical radiation from shock-heated air by using a Trailblazer II vehicle / / by Lloyd S. Keafer, Jr., and Ernest E. Burcher
| A flight measurement of optical radiation from shock-heated air by using a Trailblazer II vehicle / / by Lloyd S. Keafer, Jr., and Ernest E. Burcher |
| Autore | Keafer Lloyd S. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968 |
| Descrizione fisica | 1 online resource (38 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Trailblazer 2 reentry vehicle
Nonequilibrium radiation Aerospace vehicles Aerodynamic heating Optical radiometry Space vehicles - Atmospheric entry |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716092203321 |
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Keafer Lloyd S.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Heating and flow-field studies on a straight-wing hypersonic reentry vehicle at angles of attack from 20 ̊to 80 ̊with simulation of real-gas trends / / by James L. Hunt and Robert A. Jones
| Heating and flow-field studies on a straight-wing hypersonic reentry vehicle at angles of attack from 20 ̊to 80 ̊with simulation of real-gas trends / / by James L. Hunt and Robert A. Jones |
| Autore | Hunt James L (James Larry), <1939-> |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , March 1973 |
| Descrizione fisica | 1 online resource (94 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerospace vehicles
Hypersonic reentry Space vehicles - Atmospheric entry Aerodynamic heating Aerodynamics, Hypersonic Space shuttles Gases, Real Space vehicles - Aerodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716581803321 |
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Hunt James L (James Larry), <1939->
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| Washington, D.C. : , : National Aeronautics and Space Administration, , March 1973 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Lee-surface heating and flow phenomena on space shuttle orbiters at large angles of attack and hypersonic speeds / / by Jerry N. Hefner
| Lee-surface heating and flow phenomena on space shuttle orbiters at large angles of attack and hypersonic speeds / / by Jerry N. Hefner |
| Autore | Hefner Jerry N. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , November 1972 |
| Descrizione fisica | 1 online resource (42 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerospace vehicles
Aerodynamic heating Aerothermodynamics Space vehicles - Atmospheric entry Space shuttles Heat - Transmission Vortex-motion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716670203321 |
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Hefner Jerry N.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , November 1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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