Developments in high-speed vehicle propulsion systems [[electronic resource] /] / edited by S.N.B. Murthy, E.T. Curran |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1996 |
Descrizione fisica | 1 online resource (698 p.) |
Disciplina | 629.1/34353 |
Altri autori (Persone) |
MurthyS. N. B
CurranE. T |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Propulsion systems
High-speed aeronautics |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-640-9
1-60086-421-X |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Introduction""; ""Chapter 1. Optimal Aerodynamic Shapes of a Hypersonic Vehicle with an Airbreathing Engine""; ""Chapter 2. Low-Speed Operation of an Integrated Rocket-Ram-Scramjet for a Transatmospheric Accelerator""; ""Chapter 3. Variable Cycle Engine Developments at General Electric -1955-1995""; ""Chapter 4. Turboramjets and Installation""; ""Chapter 5. Turboramjets: Theoretical and Experimental Research at Central Institute of Aviation Motors""; ""Chapter 6. Development Study on Air Turboramjet""
""Chapter 7. In-Flight Oxidizer Collection Systems for Airbreathing Space Boosters""""Chapter 8. Air Collection Systems""; ""Chapter 9. Pulse Detonation Engine Theory And Concepts""; ""Chapter 10. Analysis of the Pulse Detonation Wave Engine""; ""Chapter 11. High-Speed Flight Thermal Management""; ""Chapter 12. Energy Management and Vehicle Synthesis""; ""Author Index"" |
Record Nr. | UNINA-9910456960703321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1996 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Developments in high-speed vehicle propulsion systems [[electronic resource] /] / edited by S.N.B. Murthy, E.T. Curran |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1996 |
Descrizione fisica | 1 online resource (698 p.) |
Disciplina | 629.1/34353 |
Altri autori (Persone) |
MurthyS. N. B
CurranE. T |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Propulsion systems
High-speed aeronautics |
ISBN |
1-60086-640-9
1-60086-421-X |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Introduction""; ""Chapter 1. Optimal Aerodynamic Shapes of a Hypersonic Vehicle with an Airbreathing Engine""; ""Chapter 2. Low-Speed Operation of an Integrated Rocket-Ram-Scramjet for a Transatmospheric Accelerator""; ""Chapter 3. Variable Cycle Engine Developments at General Electric -1955-1995""; ""Chapter 4. Turboramjets and Installation""; ""Chapter 5. Turboramjets: Theoretical and Experimental Research at Central Institute of Aviation Motors""; ""Chapter 6. Development Study on Air Turboramjet""
""Chapter 7. In-Flight Oxidizer Collection Systems for Airbreathing Space Boosters""""Chapter 8. Air Collection Systems""; ""Chapter 9. Pulse Detonation Engine Theory And Concepts""; ""Chapter 10. Analysis of the Pulse Detonation Wave Engine""; ""Chapter 11. High-Speed Flight Thermal Management""; ""Chapter 12. Energy Management and Vehicle Synthesis""; ""Author Index"" |
Record Nr. | UNINA-9910781412003321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1996 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
High-speed flight propulsion systems [[electronic resource] /] / edited by S.N.B. Murthy, E.T. Curran |
Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, 1991 |
Descrizione fisica | 1 online resource (538 p.) |
Disciplina | 629.134353 |
Altri autori (Persone) |
MurthyS. N. B
CurranE. T |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Propulsion systems
High-speed aeronautics |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-610-7
1-60086-391-4 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Introduction""; ""Chapter 1 Propulsion Systems from Takeoff to High-Speed Flight""; ""Chapter 2 Propulsion System Performance and Integration for High Mach Air Breathing Flight""; ""Chapter 3 Energy Analysis of High-Speed Flight Systems""; ""Chapter 4 Waves and Thermodynamics in High Mach Number Propulsive Ducts""; ""Chapter 5 Turbulent Free Shear Layer Mixing and Combustion""; ""Chapter 6 Turbulent Mixing in Supersonic Combustion Systems""; ""Chapter 7 Mixing and Mixing Enhancement in Supersonic Reacting Flowfields""
""Chapter 8 Study of Combustion and Heat-Exchange Processes in High-Enthalpy Short-Duration Facilities""""Chapter 9 Facility Requirements for Hypersonic Propulsion System Testing""; ""Author Index"" |
Record Nr. | UNINA-9910457645903321 |
Washington, D.C., : American Institute of Aeronautics and Astronautics, 1991 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
High-speed flight propulsion systems [[electronic resource] /] / edited by S.N.B. Murthy, E.T. Curran |
Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, 1991 |
Descrizione fisica | 1 online resource (538 p.) |
Disciplina | 629.134353 |
Altri autori (Persone) |
MurthyS. N. B
CurranE. T |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Propulsion systems
High-speed aeronautics |
ISBN |
1-60086-610-7
1-60086-391-4 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Introduction""; ""Chapter 1 Propulsion Systems from Takeoff to High-Speed Flight""; ""Chapter 2 Propulsion System Performance and Integration for High Mach Air Breathing Flight""; ""Chapter 3 Energy Analysis of High-Speed Flight Systems""; ""Chapter 4 Waves and Thermodynamics in High Mach Number Propulsive Ducts""; ""Chapter 5 Turbulent Free Shear Layer Mixing and Combustion""; ""Chapter 6 Turbulent Mixing in Supersonic Combustion Systems""; ""Chapter 7 Mixing and Mixing Enhancement in Supersonic Reacting Flowfields""
""Chapter 8 Study of Combustion and Heat-Exchange Processes in High-Enthalpy Short-Duration Facilities""""Chapter 9 Facility Requirements for Hypersonic Propulsion System Testing""; ""Author Index"" |
Record Nr. | UNINA-9910781434203321 |
Washington, D.C., : American Institute of Aeronautics and Astronautics, 1991 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Numerical methods for engine-airframe integration [[electronic resource] /] / edited by S.N.B. Murthy, Gerald C. Paynter |
Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 |
Descrizione fisica | 1 online resource (555 p.) |
Disciplina |
629.134/31
629.1 s |
Altri autori (Persone) |
MurthyS. N. B
PaynterGerald C |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Airframes - Design and construction
Airplanes - Motors |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-576-3
1-60086-357-4 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter I. Fundamental Considerations""; ""Scientific Computing Environment for the 1980's""; ""Prediction of Complex Turbulent Flows: An Overview 1985""; ""A Survey of Composite Grid Generation for General Three-Dimensional Regions""; ""Numerical Solutions of the Compressible Navier-Stokes Equations""; ""Chapter II. Scope and Opportunities""; ""Elements of Computational Engine/Airframe Integration""; ""Computational Requirements for Efficient Engine Installation""
""Application of CAE and CFD Techniques to Complete Tactical Missile Design"" ""Chapter III. Inviscid and Inviscid Plus Boundary-Layer Methods""; ""CFD Applications to Engine/Airframe Integration""; ""Three-Dimensional Flow Analysis of Turboprop Inlet and Nacelle Configurations""; ""Application of Computational Methods to the Design of Large Turbofan Engine Nacelles""; ""Comparison of Full Potential and Euler Solution Algorithms for Aeropropulsive Flowfield Computations""; ""Subsonic/Transonic/Supersonic Nozzle Flows and Nozzle Integration"" ""Chapter IV. Viscous/Inviscid Interaction and Navier-Stokes Methods"" ""Subsonic/Transonic Prediction Capabilities for Nozzle/Afterbody Configurations""; ""Three-Dimensional Viscous Design Methodology of Supersonic Inlet Systems for Advanced Technology Aircraft""; ""Review of Inlet/Airframe Integration Using Navier-Stokes Computational Fluid Dynamics""; ""Chapter V. Summary and Conclusions""; ""CFD A User's Technology Assessment""; ""Author Index"" |
Record Nr. | UNINA-9910457214703321 |
New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Numerical methods for engine-airframe integration [[electronic resource] /] / edited by S.N.B. Murthy, Gerald C. Paynter |
Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 |
Descrizione fisica | 1 online resource (555 p.) |
Disciplina |
629.134/31
629.1 s |
Altri autori (Persone) |
MurthyS. N. B
PaynterGerald C |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Airframes - Design and construction
Airplanes - Motors |
ISBN |
1-60086-576-3
1-60086-357-4 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter I. Fundamental Considerations""; ""Scientific Computing Environment for the 1980's""; ""Prediction of Complex Turbulent Flows: An Overview 1985""; ""A Survey of Composite Grid Generation for General Three-Dimensional Regions""; ""Numerical Solutions of the Compressible Navier-Stokes Equations""; ""Chapter II. Scope and Opportunities""; ""Elements of Computational Engine/Airframe Integration""; ""Computational Requirements for Efficient Engine Installation""
""Application of CAE and CFD Techniques to Complete Tactical Missile Design"" ""Chapter III. Inviscid and Inviscid Plus Boundary-Layer Methods""; ""CFD Applications to Engine/Airframe Integration""; ""Three-Dimensional Flow Analysis of Turboprop Inlet and Nacelle Configurations""; ""Application of Computational Methods to the Design of Large Turbofan Engine Nacelles""; ""Comparison of Full Potential and Euler Solution Algorithms for Aeropropulsive Flowfield Computations""; ""Subsonic/Transonic/Supersonic Nozzle Flows and Nozzle Integration"" ""Chapter IV. Viscous/Inviscid Interaction and Navier-Stokes Methods"" ""Subsonic/Transonic Prediction Capabilities for Nozzle/Afterbody Configurations""; ""Three-Dimensional Viscous Design Methodology of Supersonic Inlet Systems for Advanced Technology Aircraft""; ""Review of Inlet/Airframe Integration Using Navier-Stokes Computational Fluid Dynamics""; ""Chapter V. Summary and Conclusions""; ""CFD A User's Technology Assessment""; ""Author Index"" |
Record Nr. | UNINA-9910781405503321 |
New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Scramjet propulsion [[electronic resource] /] / edited by E.T. Curran, S.N.B. Murthy |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2000 |
Descrizione fisica | 1 online resource (1324 p.) |
Disciplina |
629.1 s
629.134/3535 |
Altri autori (Persone) |
CurranE. T
MurthyS. N. B |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Airplanes - Scramjet engines
Jet propulsion |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-660-3
1-60086-441-4 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Contents""; ""Preface""; ""Introduction""; ""I. International Efforts""; ""II. Inlets, Combustors, and Fuels""; ""III. Overall Systems""; ""IV. Future Developments""; ""V. Closing Comments""; ""References""; ""Chapter 1 Scramjet Testing in the T3 and T4 Hypersonic Impulse Facilities""; ""Nomenclature""; ""I. History, Aims, and Developments""; ""II. Facility and Instrumentation""; ""III. Fuel-Injection Systems""; ""A. Wall-Injection Combustion Results""; ""B. Wall-Injection Film-Cooling Results""; ""C. Port-Injection Results""; ""D. Central Injection""
""IV. Combustion/Mixing Processes""""A. Mixing Controlled Combustion""; ""B. Kinetically Controlled Combustion""; ""C. Shock-Induced Ignition""; ""D. Shock-Induced Mixing""; ""V. Simple Theoretical Combustor and Thrust Model""; ""VI. Experimental Results of Specific Impulse""; ""VII. Effects of Atomic Oxygen and Nitric Oxide in the Freestream""; ""VIII. Different Fuels""; ""A. Hydrocarbon Fuels""; ""B. Silane-Enriched Fuels""; ""IX. Integrated Scramjet Measurements""; ""X. Skin-Friction Measurements""; ""XI. Discussion and Review""; ""Acknowledgments""; ""Bibliography"" ""Chapter 2 Scramjet Developments in France""""I. Historical Overview""; ""II. Basic Research on Diffusion Flame Combustion (1962�1967)""; ""A. Combustion in a Cylindrical Duct""; ""B. Freejet Test""; ""C. Combustion in a Divergent Duct""; ""D. Synthesis""; ""III. ESOPE Program (1966�1973)""; ""A. Origin and Principal Aims""; ""B. Studies Results""; ""C. Synthesis""; ""IV. Studies on Shock-Induced Combustion""; ""A. Principle""; ""B. ENSMA and LATECAM Studies""; ""V. Prepha Program (1992�1997)""; ""A. Origin and Principal Aims""; ""B. System Studies"" ""C. Development of New Test Facilities""""D. Numerical Means""; ""E. Development of Scramjet Components""; ""Color Plates""; ""F. Materials and Cooled Structures""; ""G. Flight Testing""; ""VI. Perspectives""; ""A. Space Application""; ""B. Missile Application""; ""References""; ""Chapter 3 Scramjet Investigations Within the German Hypersonics Technology Program (1993�1996)""; ""I. German Hypersonics Technology Program and Scramjet-Related Activities""; ""A. German Hypersonics Technology Program""; ""B. Scramjet Related Activities Within the HTP"" ""II. Theoretical Investigations for Scramjet Intake Designs""""A. Activities at Dasa-MT633""; ""B. Activities at RWTH Aachen""; ""III. Theoretical and Experimental Investigations of Scramjet Combustion at TsAGI and DLR Lampoldshausen""; ""A. Combustor Model Design""; ""B. Fuel-Injection Modules""; ""C. Test Results""; ""IV. Freejet Wind-tunnel Testing of Scramjet Propulsion Systems at TsAGI""; ""A. Scramjet Propulsion System Model Concept""; ""B. Testing Focus""; ""C. Test Results""; ""V. Considerations for Flight Testing Small-Scale Scramjet Modules Using the RADUGA-D2 Flying Testbed"" ""A. Objectives for Flight Testing"" |
Record Nr. | UNINA-9910457546903321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, c2000 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Scramjet propulsion [[electronic resource] /] / edited by E.T. Curran, S.N.B. Murthy |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2000 |
Descrizione fisica | 1 online resource (1324 p.) |
Disciplina |
629.1 s
629.134/3535 |
Altri autori (Persone) |
CurranE. T
MurthyS. N. B |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Airplanes - Scramjet engines
Jet propulsion |
ISBN |
1-60086-660-3
1-60086-441-4 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Contents""; ""Preface""; ""Introduction""; ""I. International Efforts""; ""II. Inlets, Combustors, and Fuels""; ""III. Overall Systems""; ""IV. Future Developments""; ""V. Closing Comments""; ""References""; ""Chapter 1 Scramjet Testing in the T3 and T4 Hypersonic Impulse Facilities""; ""Nomenclature""; ""I. History, Aims, and Developments""; ""II. Facility and Instrumentation""; ""III. Fuel-Injection Systems""; ""A. Wall-Injection Combustion Results""; ""B. Wall-Injection Film-Cooling Results""; ""C. Port-Injection Results""; ""D. Central Injection""
""IV. Combustion/Mixing Processes""""A. Mixing Controlled Combustion""; ""B. Kinetically Controlled Combustion""; ""C. Shock-Induced Ignition""; ""D. Shock-Induced Mixing""; ""V. Simple Theoretical Combustor and Thrust Model""; ""VI. Experimental Results of Specific Impulse""; ""VII. Effects of Atomic Oxygen and Nitric Oxide in the Freestream""; ""VIII. Different Fuels""; ""A. Hydrocarbon Fuels""; ""B. Silane-Enriched Fuels""; ""IX. Integrated Scramjet Measurements""; ""X. Skin-Friction Measurements""; ""XI. Discussion and Review""; ""Acknowledgments""; ""Bibliography"" ""Chapter 2 Scramjet Developments in France""""I. Historical Overview""; ""II. Basic Research on Diffusion Flame Combustion (1962�1967)""; ""A. Combustion in a Cylindrical Duct""; ""B. Freejet Test""; ""C. Combustion in a Divergent Duct""; ""D. Synthesis""; ""III. ESOPE Program (1966�1973)""; ""A. Origin and Principal Aims""; ""B. Studies Results""; ""C. Synthesis""; ""IV. Studies on Shock-Induced Combustion""; ""A. Principle""; ""B. ENSMA and LATECAM Studies""; ""V. Prepha Program (1992�1997)""; ""A. Origin and Principal Aims""; ""B. System Studies"" ""C. Development of New Test Facilities""""D. Numerical Means""; ""E. Development of Scramjet Components""; ""Color Plates""; ""F. Materials and Cooled Structures""; ""G. Flight Testing""; ""VI. Perspectives""; ""A. Space Application""; ""B. Missile Application""; ""References""; ""Chapter 3 Scramjet Investigations Within the German Hypersonics Technology Program (1993�1996)""; ""I. German Hypersonics Technology Program and Scramjet-Related Activities""; ""A. German Hypersonics Technology Program""; ""B. Scramjet Related Activities Within the HTP"" ""II. Theoretical Investigations for Scramjet Intake Designs""""A. Activities at Dasa-MT633""; ""B. Activities at RWTH Aachen""; ""III. Theoretical and Experimental Investigations of Scramjet Combustion at TsAGI and DLR Lampoldshausen""; ""A. Combustor Model Design""; ""B. Fuel-Injection Modules""; ""C. Test Results""; ""IV. Freejet Wind-tunnel Testing of Scramjet Propulsion Systems at TsAGI""; ""A. Scramjet Propulsion System Model Concept""; ""B. Testing Focus""; ""C. Test Results""; ""V. Considerations for Flight Testing Small-Scale Scramjet Modules Using the RADUGA-D2 Flying Testbed"" ""A. Objectives for Flight Testing"" |
Record Nr. | UNINA-9910781422703321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, c2000 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|