37th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference : April 15-17, 1996, Salt Lake City, UT : a collection of technical papers / <general chair Dr. Kunigal Shivakumar, technical program chair William Westphal> |
Pubbl/distr/stampa | Reston, Va : American Institute of Aeronautics and Astronautics, c1996 |
Descrizione fisica | 4 v. : ill. ; 28 cm |
ISBN | 1-56347-209-0 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-990008787060403321 |
Reston, Va : American Institute of Aeronautics and Astronautics, c1996 | ||
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Lo trovi qui: Univ. Federico II | ||
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4. AIAA/CEAS Aeroacoustics conference ( 19. AIAA Aeroacoustics conference) : June 2-4, 1998, Toulouse, France : a collection of technical papers / AIAA |
Autore | American Institute of Aeronautics and Astronautics |
Pubbl/distr/stampa | Reston : American Institute of Aeronautics and Astronautics, c1998 |
Descrizione fisica | 2 v. : ill. ; 24 cm |
ISBN | 1-56347-267-8 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-990008823730403321 |
American Institute of Aeronautics and Astronautics
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Reston : American Institute of Aeronautics and Astronautics, c1998 | ||
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Lo trovi qui: Univ. Federico II | ||
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Advanced classical thermodynamics [[electronic resource] /] / George Emanuel |
Autore | Emanuel George |
Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1987 |
Descrizione fisica | 1 online resource (242 p.) |
Disciplina | 621.402/1 |
Collana | AIAA education series |
Soggetto topico | Thermodynamics |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-129-6
1-60086-001-X |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | ""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Preface""; ""Introduction""; ""Definitions and Postulates""; ""The Fundamental Equation""; ""Equilibrium""; ""Application of Jacobian Theory to Thermodynamics""; ""Maxwell's Equations""; ""Stability""; ""Theory of Real Gases""; ""Critical Point Theory""; ""Chemical Thermodynamics""; ""References""; ""SI Units""; ""Subject Index"" |
Record Nr. | UNINA-9910457543503321 |
Emanuel George
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Washington, D.C., : American Institute of Aeronautics and Astronautics, c1987 | ||
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Lo trovi qui: Univ. Federico II | ||
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Advanced classical thermodynamics / / George Emanuel |
Autore | Emanuel George |
Pubbl/distr/stampa | Washington, D.C. : , : American Institute of Aeronautics and Astronautics, , 1987 |
Descrizione fisica | 1 online resource (vii, 234 pages) : illustrations |
Disciplina | 621.402/1 |
Collana | AIAA education series |
Soggetto topico | Thermodynamics |
ISBN |
1-60086-129-6
1-60086-001-X |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | ""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Preface""; ""Introduction""; ""Definitions and Postulates""; ""The Fundamental Equation""; ""Equilibrium""; ""Application of Jacobian Theory to Thermodynamics""; ""Maxwell's Equations""; ""Stability""; ""Theory of Real Gases""; ""Critical Point Theory""; ""Chemical Thermodynamics""; ""References""; ""SI Units""; ""Subject Index"" |
Record Nr. | UNINA-9910781423403321 |
Emanuel George
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Washington, D.C. : , : American Institute of Aeronautics and Astronautics, , 1987 | ||
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Lo trovi qui: Univ. Federico II | ||
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Advanced classical thermodynamics / / George Emanuel |
Autore | Emanuel George |
Pubbl/distr/stampa | Washington, D.C. : , : American Institute of Aeronautics and Astronautics, , 1987 |
Descrizione fisica | 1 online resource (vii, 234 pages) : illustrations |
Disciplina | 621.402/1 |
Collana | AIAA education series |
Soggetto topico | Thermodynamics |
ISBN |
1-60086-129-6
1-60086-001-X |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | ""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Preface""; ""Introduction""; ""Definitions and Postulates""; ""The Fundamental Equation""; ""Equilibrium""; ""Application of Jacobian Theory to Thermodynamics""; ""Maxwell's Equations""; ""Stability""; ""Theory of Real Gases""; ""Critical Point Theory""; ""Chemical Thermodynamics""; ""References""; ""SI Units""; ""Subject Index"" |
Record Nr. | UNINA-9910828772803321 |
Emanuel George
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Washington, D.C. : , : American Institute of Aeronautics and Astronautics, , 1987 | ||
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Lo trovi qui: Univ. Federico II | ||
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Advanced hypersonic test facilities [[electronic resource] /] / edited by Frank Lu, Dan Marren |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2002 |
Descrizione fisica | 1 online resource (646 p.) |
Disciplina | 629.132306 |
Altri autori (Persone) |
LuFrank K
MarrenDan E |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Aerodynamics, Hypersonic
Hypersonic wind tunnels Ballistic ranges Rocket sleds |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-667-0
1-60086-448-1 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter 1 Hypersonic Ground Test Requirements""; ""I. Introduction""; ""II. History, Status, and Outlook for Hypersonic Test Requirements""; ""III. Potential Civilian Hypersonic Test Requirements Futures""; ""A. Planetary Exploration""; ""B. Access to Space""; ""IV. Military Hypersonic Test Requirements Futures""; ""A. Access to Space""; ""B. Missiles""; ""V. Conclusion""; ""References""; ""Chapter 2 Principles of Hypersonic Test Facility Development""; ""I. Introduction""; ""II. Critical Hypersonic Technologies""
""III. Hypersonic Scaling""""IV. High Enthalpy and High Speed""; ""V. Types of Hypersonic Facilities""; ""VI. Conclusions""; ""Acknowledgments""; ""References""; ""Chapter 3 NASA's HYPULSE Facility at GASL A Dual Mode, Dual Driver Reflected-Shock/Expansion Tunnel""; ""I. Introduction""; ""A. Background""; ""B. Scope of the Chapter""; ""II. Shock Tunnels and Expansion Tubes""; ""A. Shock-Heated Facilities""; ""B. Reflected-Shock Tunnels""; ""C. Shock-Expansion Tubes""; ""III. Driver Methods""; ""A. Lighter Gases""; ""B. Electrically Heated Light Gases"" ""C. Combustion Heated Light Gases""""D. Compressively Heated Light Gases (Free-Piston Driver)""; ""E. Summary of Comparison of Driver Techniques""; ""F. The Shock-Induced Detonation Driver for HYPULSE""; ""IV. Operation and Performance of HYPULSE""; ""A. Facility Configuration and Sizing""; ""B. HYPULSE Operation""; ""C. Test Conditions Verification""; ""D. Test Time Determination""; ""V. Driver Gas Contamination in Detonation-Driven RST Mode""; ""A. Nozzle Flow""; ""B. Transient Development of Driver-Gas Leakage""; ""VI. Nozzle Design for Expansion Tunnel Mode Operation"" ""A. Skimmer Nozzles""""B. Full Capture Contoured Inlet Asymptoting to a Conical Profile""; ""C. Verification with Experiments""; ""VII. Concluding Remarks""; ""Acknowledgments""; ""References""; ""Chapter 4 LENS Hypervelocity Tunnels and Application to Vehicle Testing at Duplicated Flight Conditions""; ""I. Introduction""; ""II. Ground Test Simulation of Hypersonic Flight Performance""; ""III. Design, Operation, and Performance of the LENS I and LENS II Hypervelocity Ground Test Facilities""; ""A. Introduction""; ""B. Design and Operation of the LENS I and II Shock Tunnels"" ""C. Aerothermal, Aero-Optic, and Radiation Instrumentation Suites""""IV. Facility Validation""; ""V. Application of Test Facility and Instrumentation to Hypersonic Vehicle Testing""; ""A. Evaluation of the Aerothermal and Aero-optical Characteristics of High-Speed Interceptors""; ""B. Examples of Aerothermal Measurements to Evaluate Seekerhead Performance""; ""C. Example of Aero-Optic Measurements on Interceptor Seekerhead Configurations""; ""VI. Measurements of Jet Interaction Resulting from Divert Thruster Operation""; ""A. Introduction""; ""B. Flowfield and Aerothermal Characteristics"" ""C. Spectrometer and Radiometer Measurements of Flowfield Obscuration Phenomena"" |
Record Nr. | UNINA-9910454412803321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, c2002 | ||
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Lo trovi qui: Univ. Federico II | ||
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Advanced hypersonic test facilities [[electronic resource] /] / edited by Frank Lu, Dan Marren |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2002 |
Descrizione fisica | 1 online resource (646 p.) |
Disciplina | 629.132306 |
Altri autori (Persone) |
LuFrank K
MarrenDan E |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Aerodynamics, Hypersonic
Hypersonic wind tunnels Ballistic ranges Rocket sleds |
ISBN |
1-60086-667-0
1-60086-448-1 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter 1 Hypersonic Ground Test Requirements""; ""I. Introduction""; ""II. History, Status, and Outlook for Hypersonic Test Requirements""; ""III. Potential Civilian Hypersonic Test Requirements Futures""; ""A. Planetary Exploration""; ""B. Access to Space""; ""IV. Military Hypersonic Test Requirements Futures""; ""A. Access to Space""; ""B. Missiles""; ""V. Conclusion""; ""References""; ""Chapter 2 Principles of Hypersonic Test Facility Development""; ""I. Introduction""; ""II. Critical Hypersonic Technologies""
""III. Hypersonic Scaling""""IV. High Enthalpy and High Speed""; ""V. Types of Hypersonic Facilities""; ""VI. Conclusions""; ""Acknowledgments""; ""References""; ""Chapter 3 NASA's HYPULSE Facility at GASL A Dual Mode, Dual Driver Reflected-Shock/Expansion Tunnel""; ""I. Introduction""; ""A. Background""; ""B. Scope of the Chapter""; ""II. Shock Tunnels and Expansion Tubes""; ""A. Shock-Heated Facilities""; ""B. Reflected-Shock Tunnels""; ""C. Shock-Expansion Tubes""; ""III. Driver Methods""; ""A. Lighter Gases""; ""B. Electrically Heated Light Gases"" ""C. Combustion Heated Light Gases""""D. Compressively Heated Light Gases (Free-Piston Driver)""; ""E. Summary of Comparison of Driver Techniques""; ""F. The Shock-Induced Detonation Driver for HYPULSE""; ""IV. Operation and Performance of HYPULSE""; ""A. Facility Configuration and Sizing""; ""B. HYPULSE Operation""; ""C. Test Conditions Verification""; ""D. Test Time Determination""; ""V. Driver Gas Contamination in Detonation-Driven RST Mode""; ""A. Nozzle Flow""; ""B. Transient Development of Driver-Gas Leakage""; ""VI. Nozzle Design for Expansion Tunnel Mode Operation"" ""A. Skimmer Nozzles""""B. Full Capture Contoured Inlet Asymptoting to a Conical Profile""; ""C. Verification with Experiments""; ""VII. Concluding Remarks""; ""Acknowledgments""; ""References""; ""Chapter 4 LENS Hypervelocity Tunnels and Application to Vehicle Testing at Duplicated Flight Conditions""; ""I. Introduction""; ""II. Ground Test Simulation of Hypersonic Flight Performance""; ""III. Design, Operation, and Performance of the LENS I and LENS II Hypervelocity Ground Test Facilities""; ""A. Introduction""; ""B. Design and Operation of the LENS I and II Shock Tunnels"" ""C. Aerothermal, Aero-Optic, and Radiation Instrumentation Suites""""IV. Facility Validation""; ""V. Application of Test Facility and Instrumentation to Hypersonic Vehicle Testing""; ""A. Evaluation of the Aerothermal and Aero-optical Characteristics of High-Speed Interceptors""; ""B. Examples of Aerothermal Measurements to Evaluate Seekerhead Performance""; ""C. Example of Aero-Optic Measurements on Interceptor Seekerhead Configurations""; ""VI. Measurements of Jet Interaction Resulting from Divert Thruster Operation""; ""A. Introduction""; ""B. Flowfield and Aerothermal Characteristics"" ""C. Spectrometer and Radiometer Measurements of Flowfield Obscuration Phenomena"" |
Record Nr. | UNINA-9910782754203321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, c2002 | ||
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Lo trovi qui: Univ. Federico II | ||
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Advanced hypersonic test facilities [[electronic resource] /] / edited by Frank Lu, Dan Marren |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2002 |
Descrizione fisica | 1 online resource (646 p.) |
Disciplina | 629.132306 |
Altri autori (Persone) |
LuFrank K
MarrenDan E |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Aerodynamics, Hypersonic
Hypersonic wind tunnels Ballistic ranges Rocket sleds |
ISBN |
1-60086-667-0
1-60086-448-1 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter 1 Hypersonic Ground Test Requirements""; ""I. Introduction""; ""II. History, Status, and Outlook for Hypersonic Test Requirements""; ""III. Potential Civilian Hypersonic Test Requirements Futures""; ""A. Planetary Exploration""; ""B. Access to Space""; ""IV. Military Hypersonic Test Requirements Futures""; ""A. Access to Space""; ""B. Missiles""; ""V. Conclusion""; ""References""; ""Chapter 2 Principles of Hypersonic Test Facility Development""; ""I. Introduction""; ""II. Critical Hypersonic Technologies""
""III. Hypersonic Scaling""""IV. High Enthalpy and High Speed""; ""V. Types of Hypersonic Facilities""; ""VI. Conclusions""; ""Acknowledgments""; ""References""; ""Chapter 3 NASA's HYPULSE Facility at GASL A Dual Mode, Dual Driver Reflected-Shock/Expansion Tunnel""; ""I. Introduction""; ""A. Background""; ""B. Scope of the Chapter""; ""II. Shock Tunnels and Expansion Tubes""; ""A. Shock-Heated Facilities""; ""B. Reflected-Shock Tunnels""; ""C. Shock-Expansion Tubes""; ""III. Driver Methods""; ""A. Lighter Gases""; ""B. Electrically Heated Light Gases"" ""C. Combustion Heated Light Gases""""D. Compressively Heated Light Gases (Free-Piston Driver)""; ""E. Summary of Comparison of Driver Techniques""; ""F. The Shock-Induced Detonation Driver for HYPULSE""; ""IV. Operation and Performance of HYPULSE""; ""A. Facility Configuration and Sizing""; ""B. HYPULSE Operation""; ""C. Test Conditions Verification""; ""D. Test Time Determination""; ""V. Driver Gas Contamination in Detonation-Driven RST Mode""; ""A. Nozzle Flow""; ""B. Transient Development of Driver-Gas Leakage""; ""VI. Nozzle Design for Expansion Tunnel Mode Operation"" ""A. Skimmer Nozzles""""B. Full Capture Contoured Inlet Asymptoting to a Conical Profile""; ""C. Verification with Experiments""; ""VII. Concluding Remarks""; ""Acknowledgments""; ""References""; ""Chapter 4 LENS Hypervelocity Tunnels and Application to Vehicle Testing at Duplicated Flight Conditions""; ""I. Introduction""; ""II. Ground Test Simulation of Hypersonic Flight Performance""; ""III. Design, Operation, and Performance of the LENS I and LENS II Hypervelocity Ground Test Facilities""; ""A. Introduction""; ""B. Design and Operation of the LENS I and II Shock Tunnels"" ""C. Aerothermal, Aero-Optic, and Radiation Instrumentation Suites""""IV. Facility Validation""; ""V. Application of Test Facility and Instrumentation to Hypersonic Vehicle Testing""; ""A. Evaluation of the Aerothermal and Aero-optical Characteristics of High-Speed Interceptors""; ""B. Examples of Aerothermal Measurements to Evaluate Seekerhead Performance""; ""C. Example of Aero-Optic Measurements on Interceptor Seekerhead Configurations""; ""VI. Measurements of Jet Interaction Resulting from Divert Thruster Operation""; ""A. Introduction""; ""B. Flowfield and Aerothermal Characteristics"" ""C. Spectrometer and Radiometer Measurements of Flowfield Obscuration Phenomena"" |
Record Nr. | UNINA-9910827022103321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, c2002 | ||
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Lo trovi qui: Univ. Federico II | ||
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Advanced propulsion systems and technologies, today to 2020 [[electronic resource] /] / edited by Claudio Bruno, Antonio G. Accettura |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2008 |
Descrizione fisica | 1 online resource (506 p.) |
Disciplina | 629.475 |
Altri autori (Persone) |
BrunoClaudio
AccetturaAntonio G |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Space vehicles - Propulsion systems
Propulsion systems |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-693-X
1-60086-474-0 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Introduction -- Advanced solid rocket motors -- Advanced cryogenic engines -- Advanced LOX-HC engines for boosters and upper stages -- LOX-hydrocarbon engines in Russia -- Green propellants -- Green propellants in Russia -- Miniaturized propulsion -- Solar thermal propulsion for upper stages -- Electric-propulsion systems -- Superconductivity -- The case for nuclear propulsion : the Rubbia's engine -- VASIMR prefeasibility analysis -- Laser propulsion systems -- Mass accelerators : Maglev and Railguns -- Solar sails : propellantless propulsion for near- and medium-term deep-space missions -- In situ resource utilization. |
Record Nr. | UNINA-9910464569303321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, c2008 | ||
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Lo trovi qui: Univ. Federico II | ||
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Advanced propulsion systems and technologies, today to 2020 / edited by Caludio Bruno, Antonio G. Accettura |
Pubbl/distr/stampa | Reston, Va. : American Institute of Aeronautics and Astronautics, c2008 |
Descrizione fisica | xiv, 489 p. : ill. ; 24 cm |
Disciplina | 629.475 |
Altri autori (Persone) |
Bruno, Claudio
Accettura, Antonio G |
Altri autori (Enti) |
American Institute of Aeronautics and Astronautics
European Space Agency |
Collana | Progress in astronautics and aeronautics ; v. 223. |
Soggetto topico | Space vehicles - Propulsion systems |
ISBN |
156347929X
9781563479298 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNISALENTO-991000093899707536 |
Reston, Va. : American Institute of Aeronautics and Astronautics, c2008 | ||
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Lo trovi qui: Univ. del Salento | ||
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