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Acoustical and flowfield characterization of a scaled tabletop rocket / / Max Kandula [and three others]
| Acoustical and flowfield characterization of a scaled tabletop rocket / / Max Kandula [and three others] |
| Autore | Kandula Max |
| Pubbl/distr/stampa | Kennedy Space Center, Florida : , : National Aeronautics and Space Administration, John F. Kennedy Space Center, , July 2001 |
| Descrizione fisica | 1 online resource (v, 16 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Acoustics
Computational fluid dynamics Rocket engines Pressure oscillations Flow distribution Combustion products |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706590103321 |
Kandula Max
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| Kennedy Space Center, Florida : , : National Aeronautics and Space Administration, John F. Kennedy Space Center, , July 2001 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerothermodynamics of gas turbine and rocket propulsion [[electronic resource] /] / Gordon C. Oates
| Aerothermodynamics of gas turbine and rocket propulsion [[electronic resource] /] / Gordon C. Oates |
| Autore | Oates Gordon C |
| Edizione | [3rd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 |
| Descrizione fisica | 1 online resource (469 p.) |
| Disciplina | 629.134/353 |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines Rocket engines |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-134-2
1-60086-006-0 1-60119-222-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Acknowledgments""; ""Table of Contents""; ""Preface""; ""Chapter 1. Introduction""; ""1.1 Purpose""; ""1.2 Chemical Rockets""; ""1.3 Nonchemical Rockets""; ""1.4 Airbreathing Engines""; ""1.5 Summary""; ""Chapter 2. Thermodynamics and Quasi-One-Dimensional Fluid Flows""; ""2.1 Introduction""; ""2.2 Definitions""; ""2.3 The Laws of Thermodynamics""; ""2.4 The Zeroth Law of Thermodynamics""; ""2.5 The First Law of Thermodynamics""; ""2.6 The Reversible Process""; ""2.7 Derived Properties: Enthalpy and Specific Heats""
""2.8 The Second Law of Thermodynamics""""2.9 The Gibbs Equation""; ""2.10 The Gibbs Function and the Helmholtz Function""; ""2.11 Maxwell's Relations""; ""2.12 General Relationships between Properties""; ""2.13 The Perfect Gas""; ""2.14 Quasi-One-Dimensional Fluid Flows""; ""2.15 The First Law for a Flowing System�The Control Volume""; ""2.16 The Channel Flow Equations""; ""2.17 Stagnation Properties""; ""2.18 Property Variations in Channels""; ""2.19 The Nozzle Flow Equations""; ""2.20 Numerical Solutions of Equations""; ""Problems""; ""Chapter 3. Chemical Rockets""; ""3.1 Introduction"" ""3.2 Expression for the Thrust""""3.3 Acceleration of a Rocket""; ""3.4 Rocket Nozzle Performance""; ""3.5 Elementary Chemistry""; ""3.6 Determination of Chamber Conditions""; ""3.7 Nozzle Flow of a Reacting Gas""; ""3.8 Solid-Propellant Rockets""; ""Problems""; ""Chapter 4. Nonchemical Rockets""; ""4.1 Introduction""; ""4.2 The Nuclear-Heated Rocket""; ""4.3 Electrically Powered Rockets""; ""Problems""; ""Chapter 5. Ideal Cycle Analysis""; ""5.1 Introduction""; ""5.2 Notation""; ""5.3 Ideal Component Behaviors""; ""5.4 The Ideal Thermodynamic Cycle"" ""5.5 The Effect of Burning at Finite Mach Number""""5.6 The Propulsive Efficiency, η[sub(p)]""; ""5.7 Systems of Units""; ""5.8 The Ideal Turbojet""; ""5.9 Interpretation of the Behavior of the Specific Fuel Consumption""; ""5.10 The Maximum Thrust Turbojet""; ""5.11 The Ideal Turbojet with Afterburning""; ""5.12 The Turbofan with Separate Exhaust Streams""; ""5.13 The Ideal Turbofan with Mixed Exhaust Streams""; ""5.14 The Ideal Constant-Pressure Mixer""; ""5.15 The Ideal Turbofan with Afterburning""; ""Problems""; ""Chapter 6. Component Performance""; ""6.1 Introduction"" ""6.2 The Thrust Equation""""6.3 Averages""; ""6.4 The Inlet""; ""6.5 The Compressor""; ""6.6 The Burner""; ""6.7 The Turbine""; ""6.8 The Nozzle""; ""6.9 Summary of Component Figures of Merit""; ""Problems""; ""Chapter 7. Nonideal Cycle Analysis""; ""7.1 Introduction""; ""7.2 The Turbojet""; ""7.3 The Turbofan""; ""7.4 The Turboprop or Prop Fan""; ""7.5 The Effects of Nonconstant Specific Heats""; ""7.6 Summary and Conclusions""; ""Problems""; ""Chapter 8. Engine Off-Design Performance""; ""8.1 Introduction""; ""8.2 Off-Design Analysis of the Turbojet"" ""8.3 Off-Design Analysis of the Turbofan"" |
| Record Nr. | UNINA-9910451105603321 |
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Oates Gordon C
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| Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerothermodynamics of gas turbine and rocket propulsion [[electronic resource] /] / Gordon C. Oates
| Aerothermodynamics of gas turbine and rocket propulsion [[electronic resource] /] / Gordon C. Oates |
| Autore | Oates Gordon C |
| Edizione | [3rd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 |
| Descrizione fisica | 1 online resource (469 p.) |
| Disciplina | 629.134/353 |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines Rocket engines |
| ISBN |
1-60086-134-2
1-60086-006-0 1-60119-222-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Acknowledgments""; ""Table of Contents""; ""Preface""; ""Chapter 1. Introduction""; ""1.1 Purpose""; ""1.2 Chemical Rockets""; ""1.3 Nonchemical Rockets""; ""1.4 Airbreathing Engines""; ""1.5 Summary""; ""Chapter 2. Thermodynamics and Quasi-One-Dimensional Fluid Flows""; ""2.1 Introduction""; ""2.2 Definitions""; ""2.3 The Laws of Thermodynamics""; ""2.4 The Zeroth Law of Thermodynamics""; ""2.5 The First Law of Thermodynamics""; ""2.6 The Reversible Process""; ""2.7 Derived Properties: Enthalpy and Specific Heats""
""2.8 The Second Law of Thermodynamics""""2.9 The Gibbs Equation""; ""2.10 The Gibbs Function and the Helmholtz Function""; ""2.11 Maxwell's Relations""; ""2.12 General Relationships between Properties""; ""2.13 The Perfect Gas""; ""2.14 Quasi-One-Dimensional Fluid Flows""; ""2.15 The First Law for a Flowing System�The Control Volume""; ""2.16 The Channel Flow Equations""; ""2.17 Stagnation Properties""; ""2.18 Property Variations in Channels""; ""2.19 The Nozzle Flow Equations""; ""2.20 Numerical Solutions of Equations""; ""Problems""; ""Chapter 3. Chemical Rockets""; ""3.1 Introduction"" ""3.2 Expression for the Thrust""""3.3 Acceleration of a Rocket""; ""3.4 Rocket Nozzle Performance""; ""3.5 Elementary Chemistry""; ""3.6 Determination of Chamber Conditions""; ""3.7 Nozzle Flow of a Reacting Gas""; ""3.8 Solid-Propellant Rockets""; ""Problems""; ""Chapter 4. Nonchemical Rockets""; ""4.1 Introduction""; ""4.2 The Nuclear-Heated Rocket""; ""4.3 Electrically Powered Rockets""; ""Problems""; ""Chapter 5. Ideal Cycle Analysis""; ""5.1 Introduction""; ""5.2 Notation""; ""5.3 Ideal Component Behaviors""; ""5.4 The Ideal Thermodynamic Cycle"" ""5.5 The Effect of Burning at Finite Mach Number""""5.6 The Propulsive Efficiency, η[sub(p)]""; ""5.7 Systems of Units""; ""5.8 The Ideal Turbojet""; ""5.9 Interpretation of the Behavior of the Specific Fuel Consumption""; ""5.10 The Maximum Thrust Turbojet""; ""5.11 The Ideal Turbojet with Afterburning""; ""5.12 The Turbofan with Separate Exhaust Streams""; ""5.13 The Ideal Turbofan with Mixed Exhaust Streams""; ""5.14 The Ideal Constant-Pressure Mixer""; ""5.15 The Ideal Turbofan with Afterburning""; ""Problems""; ""Chapter 6. Component Performance""; ""6.1 Introduction"" ""6.2 The Thrust Equation""""6.3 Averages""; ""6.4 The Inlet""; ""6.5 The Compressor""; ""6.6 The Burner""; ""6.7 The Turbine""; ""6.8 The Nozzle""; ""6.9 Summary of Component Figures of Merit""; ""Problems""; ""Chapter 7. Nonideal Cycle Analysis""; ""7.1 Introduction""; ""7.2 The Turbojet""; ""7.3 The Turbofan""; ""7.4 The Turboprop or Prop Fan""; ""7.5 The Effects of Nonconstant Specific Heats""; ""7.6 Summary and Conclusions""; ""Problems""; ""Chapter 8. Engine Off-Design Performance""; ""8.1 Introduction""; ""8.2 Off-Design Analysis of the Turbojet"" ""8.3 Off-Design Analysis of the Turbofan"" |
| Record Nr. | UNINA-9910783934603321 |
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Oates Gordon C
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| Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerothermodynamics of gas turbine and rocket propulsion / / Gordon C. Oates
| Aerothermodynamics of gas turbine and rocket propulsion / / Gordon C. Oates |
| Autore | Oates Gordon C |
| Edizione | [3rd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 |
| Descrizione fisica | 1 online resource (469 p.) |
| Disciplina | 629.134/353 |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines Rocket engines |
| ISBN |
1-60086-134-2
1-60086-006-0 1-60119-222-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Acknowledgments""; ""Table of Contents""; ""Preface""; ""Chapter 1. Introduction""; ""1.1 Purpose""; ""1.2 Chemical Rockets""; ""1.3 Nonchemical Rockets""; ""1.4 Airbreathing Engines""; ""1.5 Summary""; ""Chapter 2. Thermodynamics and Quasi-One-Dimensional Fluid Flows""; ""2.1 Introduction""; ""2.2 Definitions""; ""2.3 The Laws of Thermodynamics""; ""2.4 The Zeroth Law of Thermodynamics""; ""2.5 The First Law of Thermodynamics""; ""2.6 The Reversible Process""; ""2.7 Derived Properties: Enthalpy and Specific Heats""
""2.8 The Second Law of Thermodynamics""""2.9 The Gibbs Equation""; ""2.10 The Gibbs Function and the Helmholtz Function""; ""2.11 Maxwell's Relations""; ""2.12 General Relationships between Properties""; ""2.13 The Perfect Gas""; ""2.14 Quasi-One-Dimensional Fluid Flows""; ""2.15 The First Law for a Flowing System�The Control Volume""; ""2.16 The Channel Flow Equations""; ""2.17 Stagnation Properties""; ""2.18 Property Variations in Channels""; ""2.19 The Nozzle Flow Equations""; ""2.20 Numerical Solutions of Equations""; ""Problems""; ""Chapter 3. Chemical Rockets""; ""3.1 Introduction"" ""3.2 Expression for the Thrust""""3.3 Acceleration of a Rocket""; ""3.4 Rocket Nozzle Performance""; ""3.5 Elementary Chemistry""; ""3.6 Determination of Chamber Conditions""; ""3.7 Nozzle Flow of a Reacting Gas""; ""3.8 Solid-Propellant Rockets""; ""Problems""; ""Chapter 4. Nonchemical Rockets""; ""4.1 Introduction""; ""4.2 The Nuclear-Heated Rocket""; ""4.3 Electrically Powered Rockets""; ""Problems""; ""Chapter 5. Ideal Cycle Analysis""; ""5.1 Introduction""; ""5.2 Notation""; ""5.3 Ideal Component Behaviors""; ""5.4 The Ideal Thermodynamic Cycle"" ""5.5 The Effect of Burning at Finite Mach Number""""5.6 The Propulsive Efficiency, η[sub(p)]""; ""5.7 Systems of Units""; ""5.8 The Ideal Turbojet""; ""5.9 Interpretation of the Behavior of the Specific Fuel Consumption""; ""5.10 The Maximum Thrust Turbojet""; ""5.11 The Ideal Turbojet with Afterburning""; ""5.12 The Turbofan with Separate Exhaust Streams""; ""5.13 The Ideal Turbofan with Mixed Exhaust Streams""; ""5.14 The Ideal Constant-Pressure Mixer""; ""5.15 The Ideal Turbofan with Afterburning""; ""Problems""; ""Chapter 6. Component Performance""; ""6.1 Introduction"" ""6.2 The Thrust Equation""""6.3 Averages""; ""6.4 The Inlet""; ""6.5 The Compressor""; ""6.6 The Burner""; ""6.7 The Turbine""; ""6.8 The Nozzle""; ""6.9 Summary of Component Figures of Merit""; ""Problems""; ""Chapter 7. Nonideal Cycle Analysis""; ""7.1 Introduction""; ""7.2 The Turbojet""; ""7.3 The Turbofan""; ""7.4 The Turboprop or Prop Fan""; ""7.5 The Effects of Nonconstant Specific Heats""; ""7.6 Summary and Conclusions""; ""Problems""; ""Chapter 8. Engine Off-Design Performance""; ""8.1 Introduction""; ""8.2 Off-Design Analysis of the Turbojet"" ""8.3 Off-Design Analysis of the Turbofan"" |
| Record Nr. | UNINA-9910812009403321 |
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Oates Gordon C
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| Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analytical and experimental investigation of outflow residuals in interconnected spherical tanks / / by Harold J. Kasper and Robert J. Boyle
| Analytical and experimental investigation of outflow residuals in interconnected spherical tanks / / by Harold J. Kasper and Robert J. Boyle |
| Autore | Kasper Harold J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , September 1968 |
| Descrizione fisica | 1 online resource (ii, 33 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Fluid mechanics
Rocket engines Liquid propellant rockets - Fuel tanks Rocket engines - Fuel systems Rockets (Aeronautics) - Fuel tanks |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715457803321 |
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Kasper Harold J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , September 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analytical and numerical modeling of sensor port acoustics / / M.J. Casiano, S.R. Fischbach
| Analytical and numerical modeling of sensor port acoustics / / M.J. Casiano, S.R. Fischbach |
| Autore | Casiano M. J. |
| Pubbl/distr/stampa | Huntsville, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , January 2021 |
| Descrizione fisica | 1 online resourcce (xxi, 115 pages, 1 unnumbered page) : color illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Acoustics
Rocket engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715396703321 |
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Casiano M. J.
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| Huntsville, Alabama : , : National Aeronautics and Space Administration, Marshall Space Flight Center, , January 2021 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Annular slit colloid thruster research and development / / by Kenneth W. Stark and William A. Burton
| Annular slit colloid thruster research and development / / by Kenneth W. Stark and William A. Burton |
| Autore | Stark Kenneth W. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , May 1971 |
| Descrizione fisica | 1 online resource (v, 56 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerospace vehicles
Propellants Rocket engines Rocket engines - Thrust Space vehicles - Propulsion systems |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716001703321 |
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Stark Kenneth W.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , May 1971 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Back flow from jet plumes in vacuum / / by Norman T. Grier
| Back flow from jet plumes in vacuum / / by Norman T. Grier |
| Autore | Grier Norman T. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 |
| Descrizione fisica | 1 online resource (ii, 17 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Fluid dynamics
Aerospace vehicles Rocket engines Fluid dynamics (Space environment) - Mathematical models Plumes (Fluid dynamics) - Mathematical models Space vehicles - Propulsion systems - Mathematical models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716074903321 |
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Grier Norman T.
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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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Bleed cycle propellant pumping in a gas-core nuclear rocket engine system / / by Albert F. Kascak and Annie J. Easley
| Bleed cycle propellant pumping in a gas-core nuclear rocket engine system / / by Albert F. Kascak and Annie J. Easley |
| Autore | Kascak Albert F. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , March 1972 |
| Descrizione fisica | 1 online resource (approximately 78 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Spacecraft propulsion
Spacecraft power supplies Rocket engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717038003321 |
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Kascak Albert F.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , March 1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Characterization of real gas properties for Space Shuttle main engine fuel turbine and performance calculations [[electronic resource] /] / Gary J. Harloff
| Characterization of real gas properties for Space Shuttle main engine fuel turbine and performance calculations [[electronic resource] /] / Gary J. Harloff |
| Autore | Harloff G. J (Gary James), <1945-> |
| Pubbl/distr/stampa | Cleveland, Ohio : , : Sverdrup Technology, Inc., Lewis Research Center, , [1986] |
| Descrizione fisica | 1 online resource (11 pages, 83 unnumbered pages) : illustrations |
| Collana | NASA contractor report |
| Soggetto topico |
Air
Fuel systems Hydrogen fuels Real gases Rocket engines Space Shuttle Main Engine Steam Thermodynamic properties Transport properties Turbine pumps |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701957103321 |
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Harloff G. J (Gary James), <1945->
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| Cleveland, Ohio : , : Sverdrup Technology, Inc., Lewis Research Center, , [1986] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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