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Aerothermal analysis and design of the Gravity Recovery and Climate Experiment (GRACE) spacecraft / / Daniel D. Mazanek, Renjith R. Kumar, Min Qu, and Hans Seywald
| Aerothermal analysis and design of the Gravity Recovery and Climate Experiment (GRACE) spacecraft / / Daniel D. Mazanek, Renjith R. Kumar, Min Qu, and Hans Seywald |
| Autore | Mazanek Daniel D. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2000 |
| Descrizione fisica | 1 online resource (43 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerothermodynamics
Design analysis Gravitation Climate Spacecraft design Thermal analysis Attitude control Orbital lifetime Spacecraft control |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerothermal analysis and design of the Gravity Recovery and Climate Experiment |
| Record Nr. | UNINA-9910706220103321 |
Mazanek Daniel D.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2000 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerothermal analysis of a wing-elevon cove with variable leakage / / L. Roane Hunt
| Aerothermal analysis of a wing-elevon cove with variable leakage / / L. Roane Hunt |
| Autore | Hunt L. Roane (Lewis Roane) |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980 |
| Descrizione fisica | 1 online resource (41 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Elevons
Mathematical models Reynolds number Space Shuttle orbiters Wind tunnel tests Aerothermodynamics Airplanes - Wings |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707473203321 |
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Hunt L. Roane (Lewis Roane)
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes / / Robert J. Nowak, Cindy W. Albertson, and L. Roane Hunt
| Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes / / Robert J. Nowak, Cindy W. Albertson, and L. Roane Hunt |
| Autore | Nowak Robert J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , January 1985 |
| Descrizione fisica | 1 online resource (87 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Flow distribution
Cones Aerodynamic heating Boundary layer transition Turbulent boundary layer Angle of attack (Aerodynamics) Noses (Aircraft) Reynolds number Aerothermodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709616703321 |
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Nowak Robert J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , January 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerothermodynamics of aircraft engine components [[electronic resource] /] / edited by Gordon C. Oates
| Aerothermodynamics of aircraft engine components [[electronic resource] /] / edited by Gordon C. Oates |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 |
| Descrizione fisica | 1 online resource (559 p.) |
| Disciplina | 629.134/353 |
| Altri autori (Persone) | OatesGordon C |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-133-4
1-60086-005-2 1-60119-204-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Preface""; ""Chapter 1. Fundamentals of Combustion""; ""1.1 Introduction""; ""1.2 Chemistry""; ""1.3 Thermodynamics""; ""1.4 Gasdynamics and Diffusion Processes""; ""1.5 Combustion Parameters""; ""1.6 Jet Fuels""; ""1.7 Summary""; ""Chapter 2. Afterburners""; ""2.1 Introduction""; ""2.2 Diffuser""; ""2.3 Fuel Injection, Atomization, and Vaporization""; ""2.4 Ignition""; ""2.5 Stabilization Process""; ""2.6 Flame Spread in Premixed and Homogeneous Fuel-Air Mixtures""; ""2.7 Nozzle and Fuel Control Systems""
""2.8 Complete Afterburner Systems""""2.9 Combustion Instabilities""; ""Chapter 3. Axial Flow Compressor Aerodynamics""; ""3.1 Introduction""; ""3.2 Axial Flow Compressor Nomenclature and Terminology""; ""3.3 Characteristics of the Flow in Axial Flow Compressor Configurations""; ""3.4 Aerodynamic Design Objectives for Axial Flow Compressor Units""; ""3.5 Elements of a Compressor Design System�Technical Requirements""; ""3.6 Content of Current and Developing Design Systems� The Technology Base""; ""3.7 Component and Configuration Experimental Development"" ""3.8 Axial Flow Compressor Performance Trends""""Chapter 4. Turbine Aerodynamics""; ""4.1 Introduction""; ""4.2 Turbine Airfoil Characteristics""; ""4.3 Design Considerations""; ""4.4 Performance""; ""4.5 Profile Aerodynamics""; ""4.6 End Wall Aerodynamics""; ""4.7 Parasitic Loss""; ""4.8 Structural Excitation""; ""4.9 Stage Performance""; ""4.10 Looking Ahead""; ""4.11 Looking Back�Developments Since 1977""; ""Chapter 5. Turbine Cooling""; ""5.1 Introduction""; ""5.2 Cooling Design Problem""; ""5.3 Airfoil Cooling""; ""5.4 End Wall Cooling""; ""5.5 Conclusions""; ""5.6 Recent Advances"" ""Chapter 6. Computation of Turbomachinery Boundary Layers""""6.1 Introduction""; ""6.2 Two-Dimensional or Axisymmetric Boundary Layers""; ""6.3 Three-Dimensional Boundary Layers""; ""6.4 Boundary-Layer Separation""; ""6.5 Turbulence Models""; ""6.6 Conclusion""; ""Chapter 7. Engine Noise""; ""7.1 Introduction""; ""7.2 Scales and Ratings for Noise""; ""7.3 Introduction to Acoustics of Ducts""; ""7.4 Compressor and Fan Noise""; ""7.5 Turbine Noise""; ""7.6 Core Noise""; ""7.7 Acoustic Treatment""; ""7.8 Conclusions and Future Prospects""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E"" ""F""""G""; ""H""; ""I""; ""J""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""V""; ""W"" |
| Record Nr. | UNINA-9910451071403321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerothermodynamics of aircraft engine components [[electronic resource] /] / edited by Gordon C. Oates
| Aerothermodynamics of aircraft engine components [[electronic resource] /] / edited by Gordon C. Oates |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 |
| Descrizione fisica | 1 online resource (559 p.) |
| Disciplina | 629.134/353 |
| Altri autori (Persone) | OatesGordon C |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines |
| ISBN |
1-60086-133-4
1-60086-005-2 1-60119-204-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Preface""; ""Chapter 1. Fundamentals of Combustion""; ""1.1 Introduction""; ""1.2 Chemistry""; ""1.3 Thermodynamics""; ""1.4 Gasdynamics and Diffusion Processes""; ""1.5 Combustion Parameters""; ""1.6 Jet Fuels""; ""1.7 Summary""; ""Chapter 2. Afterburners""; ""2.1 Introduction""; ""2.2 Diffuser""; ""2.3 Fuel Injection, Atomization, and Vaporization""; ""2.4 Ignition""; ""2.5 Stabilization Process""; ""2.6 Flame Spread in Premixed and Homogeneous Fuel-Air Mixtures""; ""2.7 Nozzle and Fuel Control Systems""
""2.8 Complete Afterburner Systems""""2.9 Combustion Instabilities""; ""Chapter 3. Axial Flow Compressor Aerodynamics""; ""3.1 Introduction""; ""3.2 Axial Flow Compressor Nomenclature and Terminology""; ""3.3 Characteristics of the Flow in Axial Flow Compressor Configurations""; ""3.4 Aerodynamic Design Objectives for Axial Flow Compressor Units""; ""3.5 Elements of a Compressor Design System�Technical Requirements""; ""3.6 Content of Current and Developing Design Systems� The Technology Base""; ""3.7 Component and Configuration Experimental Development"" ""3.8 Axial Flow Compressor Performance Trends""""Chapter 4. Turbine Aerodynamics""; ""4.1 Introduction""; ""4.2 Turbine Airfoil Characteristics""; ""4.3 Design Considerations""; ""4.4 Performance""; ""4.5 Profile Aerodynamics""; ""4.6 End Wall Aerodynamics""; ""4.7 Parasitic Loss""; ""4.8 Structural Excitation""; ""4.9 Stage Performance""; ""4.10 Looking Ahead""; ""4.11 Looking Back�Developments Since 1977""; ""Chapter 5. Turbine Cooling""; ""5.1 Introduction""; ""5.2 Cooling Design Problem""; ""5.3 Airfoil Cooling""; ""5.4 End Wall Cooling""; ""5.5 Conclusions""; ""5.6 Recent Advances"" ""Chapter 6. Computation of Turbomachinery Boundary Layers""""6.1 Introduction""; ""6.2 Two-Dimensional or Axisymmetric Boundary Layers""; ""6.3 Three-Dimensional Boundary Layers""; ""6.4 Boundary-Layer Separation""; ""6.5 Turbulence Models""; ""6.6 Conclusion""; ""Chapter 7. Engine Noise""; ""7.1 Introduction""; ""7.2 Scales and Ratings for Noise""; ""7.3 Introduction to Acoustics of Ducts""; ""7.4 Compressor and Fan Noise""; ""7.5 Turbine Noise""; ""7.6 Core Noise""; ""7.7 Acoustic Treatment""; ""7.8 Conclusions and Future Prospects""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E"" ""F""""G""; ""H""; ""I""; ""J""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""V""; ""W"" |
| Record Nr. | UNINA-9910783937603321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 | ||
| 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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Aerothermodynamik : Originalveröffentl. im Springer-Verl., Berlin, 1994 / / Herbert Oertel, editor
| Aerothermodynamik : Originalveröffentl. im Springer-Verl., Berlin, 1994 / / Herbert Oertel, editor |
| Pubbl/distr/stampa | [Place of publication not identified] : , : KIT Scientific Publishing, , 2005 |
| Descrizione fisica | 1 online resource (898 pages) |
| Disciplina | 629.1323 |
| Soggetto topico |
Aerothermodynamics
Aerodynamic heating |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | ger |
| Record Nr. | UNINA-9910688334303321 |
| [Place of publication not identified] : , : KIT Scientific Publishing, , 2005 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aircraft thermal management : systems architectures / / by Mark F. Ahlers
| Aircraft thermal management : systems architectures / / by Mark F. Ahlers |
| Autore | Ahlers Mark F. |
| Pubbl/distr/stampa | Warrendale, Pennsylvania (400 Commonwealth Dr., Wallendale PA USA) : , : Society of Automotive Engineers, , 2016 |
| Descrizione fisica | 1 online resource (v, 99 pages) : illustrations |
| Disciplina | 629.134 |
| Collana |
PT
Society of Automotive Engineers. Electronic publications |
| Soggetto topico |
Aerothermodynamics
Aerodynamic heating |
| ISBN |
0-7680-8726-0
0-7680-8297-8 1-5231-0631-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 1. Aircraft thermal management-heat sink challenge (2014-01-2193) / Dooley, M., Lui, N., Newman, R., and Lui, C -- 2. Integrated aircraft thermal management & power generation: Reconfiguration of a closed loop air cycle system as a Brayton cycle gas generator to support auxiliary electric power generation (2014-01-2192) / Abolmoali, P., Parrilla, J., and Hamed, A -- 3. Aircraft integration challenges and opportunities for distributed intelligent control, power, thermal management, diagnostic and prognostic systems (2014-01-2161) / Behbahani, A., Von Moll, A., Zeller, R., and Ordo, J -- 4. Thermal management investigations for fuel cell systems on-board commercial aircraft (2013-01-2274) / Vredenborg, E., and Thielecke, F -- 5. Power and thermal management for future aircraft (2013-01-2273) / Ganev, E., and Koerner, M -- 6. A highly stable two-phase thermal management system for aircraft (2012-01-2186) / Chen, W., Fogg, D., Izenson, M., and Kurwitz, C -- 7. Thermal management and power generation for directed energy weapons (2010-01-1781) / Patel, V. P., Koerner, M., Loeffelholz, D -- 8. Comparative analysis of thermal management architectures to address evolving thermal requirements of aircraft systems (2008-01-2905) / Homitz, J., Scaringe, R., Cole, G., Fleming, A., et al -- 9. Aircraft thermal management using loop heat pipes: Experimental simulation of high acceleration environments using the centrifuge table test bed (2006-01-3066) / Fleming, A., Leland, Q., Yerkes, K., Elston, L., et al -- 10. Evaluation of a vapor-compression thermal management system for reliability while operating under thermal transients (2010-01-1733) / Homitz, J., Scaringe, R., and Cole, G. |
| Record Nr. | UNINA-9910438308503321 |
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Ahlers Mark F.
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| Warrendale, Pennsylvania (400 Commonwealth Dr., Wallendale PA USA) : , : Society of Automotive Engineers, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aircraft thermal management : integrated energy system analysis / / by Mark F. Ahlers
| Aircraft thermal management : integrated energy system analysis / / by Mark F. Ahlers |
| Autore | Ahlers Mark F. |
| Pubbl/distr/stampa | Warrendale, Pennsylvania (400 Commonwealth Dr., Wallendale PA USA) : , : Society of Automotive Engineers, , 2016 |
| Descrizione fisica | 1 online resource (v, 109 pages) : illustrations, maps |
| Disciplina | 629.135 |
| Collana |
PT
Society of Automotive Engineers. Electronic publications |
| Soggetto topico |
Aerothermodynamics
Aerodynamic heating |
| ISBN |
0-7680-8727-9
0-7680-8304-4 1-5231-0632-8 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 1. An exergy-based methodology for decision-based design of integrated aircraft thermal systems (2000-01-5527) / Figliola, R., and Tipton, R -- 2. Dynamic thermal management system modeling of a more electric aircraft (2008-01-2886) / McCarthy, K., Walters, E., Heltzel, A., Elangovan, R., et. al -- 3. Facilitating the energy optimization of aircraft propulsion and thermal management systems through integrated modeling and simulation (2010-01-1787) / Maser, A., Garcia, E., and Mavris, D -- 4. Power thermal management system design for enhanced performance in an aircraft vehicle (2010-01-1805) / Bodie, M -- 5. Integrated electrical and thermal management sub-system optimization (2010-01-1812) / Bodden, D., Eller, B., and Clements, S -- 6. Thermal management investigations for fuel cell systems on-board commercial aircraft (2013-01-2274) / Vredenborg, E., and Thielecke, F -- 7. Advantages of the dynamic simulation for the thermal management systems design (2014-01-2152) / Del Valle, P., and Blazquez Munoz, P -- 8. A thermal management assessment tool for advanced hypersonic aircraft (921941) / Issacci, F., Wassel, A. Farr, J., Wallace, C., et al -- 9. Model-based thermal management functions for aircraft systems (2014-01-2203) / Schlabe, D., and Lienig, J -- 10. A modeling approach for integrated thermal management system analysis of aircraft (971242) / Van Griethuysen, V.J., Issacci, F., and Farr, J., Jr. |
| Record Nr. | UNINA-9910438308703321 |
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Ahlers Mark F.
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| Warrendale, Pennsylvania (400 Commonwealth Dr., Wallendale PA USA) : , : Society of Automotive Engineers, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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