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Advanced hypersonic test facilities [[electronic resource] /] / edited by Frank Lu, Dan Marren
| 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 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Advanced hypersonic test facilities [[electronic resource] /] / edited by Frank Lu, Dan Marren
| 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 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Advanced hypersonic test facilities / / edited by Frank Lu, Dan Marren
| Advanced hypersonic test facilities / / edited by Frank Lu, Dan Marren |
| Edizione | [1st ed.] |
| 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-9910971123903321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Elementi di aerodinamica ipersonica / Rodolfo Monti, Gennaro Zuppardi
| Elementi di aerodinamica ipersonica / Rodolfo Monti, Gennaro Zuppardi |
| Autore | Monti, Rodolfo |
| Edizione | [2 ed.] |
| Pubbl/distr/stampa | Napoli : Liguori, 2012 |
| Descrizione fisica | X, 450 p. : ill. ; 24 cm |
| Disciplina | 629.132306 |
| Altri autori (Persone) | Zuppardi, Gennaro |
| Soggetto non controllato | Volo meccanico - Dinamica |
| ISBN | 978-88-207-3328-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | ita |
| Record Nr. | UNINA-990009642860403321 |
Monti, Rodolfo
|
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| Napoli : Liguori, 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Elementi di aerodinamica ipersonica / Rodolfo Monti, Gennaro Zuppardi
| Elementi di aerodinamica ipersonica / Rodolfo Monti, Gennaro Zuppardi |
| Autore | Monti, Rodolfo <1931- > |
| Pubbl/distr/stampa | Napoli : Liguori, 2002 |
| Descrizione fisica | X, 419 p. : ill. ; 24 cm |
| Disciplina | 629.132306 |
| Altri autori (Persone) | Zuppardi, Gennaro |
| Soggetto non controllato | Volo meccanico - Dinamica |
| ISBN | 88-207-3328-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | ita |
| Record Nr. | UNINA-990000902280403321 |
|
Monti, Rodolfo <1931- >
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| Napoli : Liguori, 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Elements of Hypersonic Airbreather Design and Development
| Elements of Hypersonic Airbreather Design and Development |
| Autore | Hirschel Ernst-Heinrich |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Cham : , : Springer, , 2025 |
| Descrizione fisica | 1 online resource (382 pages) |
| Disciplina | 629.132306 |
| Altri autori (Persone) |
StaudacherWerner
HornungMirko KlicheDaniel |
| Collana | Mechanical Engineering (R0) Series |
| ISBN | 3-031-94219-1 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9911028741903321 |
|
Hirschel Ernst-Heinrich
|
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| Cham : , : Springer, , 2025 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hypersonic and supersonic flight : advances in aerodynamics, materials, and vehicle design / / edited by Konstantin Volkov
| Hypersonic and supersonic flight : advances in aerodynamics, materials, and vehicle design / / edited by Konstantin Volkov |
| Pubbl/distr/stampa | London : , : IntechOpen, , 2023 |
| Descrizione fisica | 1 online resource (180 pages) |
| Disciplina | 629.132306 |
| Soggetto topico |
Aerodynamics, Hypersonic
Aerodynamics |
| ISBN | 1-83768-260-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | 1. High-Temperature Effects on Supersonic Flow around a Wedge -- 2. Design and CFD Analysis on the Reduction of Thermal Effect in Re-entry Vehicle by Using Retractable Aerospike -- 3. Design and Performance of Hypersonic Intake for Scramjet Engine -- 4. Clean and Sustainable Hydrogen-Electric Propulsion -- 5. Cyclic Oxidation of Diffusion Aluminide Coatings -- 6. Perspective Chapter: Effect of Laser Key Parameters on the Ignition of Boron Potassium Nitrate with a Changing Working Distance. |
| Record Nr. | UNINA-9910727285803321 |
| London : , : IntechOpen, , 2023 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hypersonic curved compression inlet and its inverse design / / Kunyuan Zhang
| Hypersonic curved compression inlet and its inverse design / / Kunyuan Zhang |
| Autore | Zhang Kun-Yuan |
| Edizione | [1st edition 2020.] |
| Pubbl/distr/stampa | Singapore : , : Springer Singapore : , : Imprint : Springer, , 2020 |
| Descrizione fisica | 1 online resource (XIV, 332 p.) : 391 illus., 288 illus. in color |
| Disciplina | 629.132306 |
| Collana | Advanced Topics in Science and Technology in China |
| Soggetto topico |
Aerodynamics, Hypersonic
Curves Fluid- and Aerodynamics Engineering Fluid Dynamics Aerospace Technology and Astronautics |
| ISBN | 981-15-0727-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field -- Forward Design of Two Dimensional Curved Shock Wave Curved Compression Surface -- Inverse Design of Compression Inlet with Specified Exit Aerodynamic Parameters -- Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design of Axisymmetric Reference Flow Field on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet -- Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet -- Features and Drag Reduction Analysis of Drag in Hypersonic Inlet -- The Development of Curved Compression and Application Prospect. |
| Record Nr. | UNINA-9910373956303321 |
|
Zhang Kun-Yuan
|
||
| Singapore : , : Springer Singapore : , : Imprint : Springer, , 2020 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Hypersonic curved compression inlet and its inverse design / / Kunyuan Zhang
| Hypersonic curved compression inlet and its inverse design / / Kunyuan Zhang |
| Autore | Zhang Kun-Yuan |
| Edizione | [1st edition 2020.] |
| Pubbl/distr/stampa | Singapore : , : Springer Singapore : , : Imprint : Springer, , 2020 |
| Descrizione fisica | 1 online resource (XIV, 332 p.) : 391 illus., 288 illus. in color |
| Disciplina | 629.132306 |
| Collana | Advanced Topics in Science and Technology in China |
| Soggetto topico |
Aerodynamics, Hypersonic
Curves Fluid- and Aerodynamics Engineering Fluid Dynamics Aerospace Technology and Astronautics |
| ISBN | 981-15-0727-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Introduction -- Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field -- Forward Design of Two Dimensional Curved Shock Wave Curved Compression Surface -- Inverse Design of Compression Inlet with Specified Exit Aerodynamic Parameters -- Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design of Axisymmetric Reference Flow Field on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet -- Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet -- Features and Drag Reduction Analysis of Drag in Hypersonic Inlet -- The Development of Curved Compression and Application Prospect. |
| Record Nr. | UNISA-996418170303316 |
|
Zhang Kun-Yuan
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| Singapore : , : Springer Singapore : , : Imprint : Springer, , 2020 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. di Salerno | ||
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Hypersonic Inviscid Flow
| Hypersonic Inviscid Flow |
| Autore | Hayes Wallace D |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Newburyport, : Dover Publications, 2012 |
| Descrizione fisica | 1 online resource (1074 p.) |
| Disciplina |
629.132
629.132306 |
| Altri autori (Persone) | ProbsteinRonald F |
| Collana | Dover Books on Physics |
| Soggetto topico |
Aerodynamics, Hypersonic
Air flow -- Mathematical models Inviscid flow |
| ISBN |
1-5231-0964-5
0-486-16048-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Title Page; Copyright Page; Dedication; PREFACE TO THE DOVER EDITION; PREFACE TO VOLUME I; PREFACE TO THE FIRST EDITION; Table of Contents; Erratum; CHAPTER I - GENERAL CONSIDERATIONS; 1. Introductory remarks; 2. General features of hypersonic flow fields; 3. Assumptions underlying inviscid hypersonic theory; 4. The normal shock wave; 5. Oblique and curved shocks; 6. Mach number independence principle; 7. General strip theory; 8. Dissipative effects; CHAPTER II - SMALL-DISTURBANCE THEORY; 1. Introduction and basic equations; 2. Hypersonic similitude
3. Unified supersonic-hypersonic similitude4. Slender-body strip theory; 5. Examples of small-disturbance solutions; 6. Similar power-law solutions; 7. Application of similar solutions to steady flows; 8. Slightly blunted slender bodies; 9. Large incidence and correlation of similitudes; 10. Unsteady flow theory; 11. Nonequilibrium effects; CHAPTER III - NEWTONIAN THEORY; 1. The gasdynamics of Sir Isaac Newton; 2. Two-dimensional and axisymmetric bodies; 3. Simple shapes and free layers; 4. Optimum shapes; 5. Shock layer structure and cross flow phenomena 6. Shock layer structure with cross flow7. Conical flow; 8. Bodies of revolution at small incidence; 9. Unsteady flow; CHAPTER IV - CONSTANT-DENSITY SOLUTIONS; 1. The wedge; 2. The cone; 3. Circular cylinder; 4. The sphere; 5. Solutions with cross flow; CHAPTER V - THE THEORY OF THIN SHOCK LAYERS; 1. Basic concepts; 2. Successive approximation schemes; 3. Constant-streamtube-area approximation; 4. Two-dimensional and axisymmetric blunt-faced bodies; 5. Quasi wedges and quasi cones; 6. Conical bodies; 7. General blunt-faced bodies and related similitudes; 8. Integral methods 9. Newtonian separation10. Nonequilibrium flows; CHAPTER VI - NUMERICAL METHODS FOR BLUNT-BODY FLOWS; 1. Nature of the problem; 2. Streamtube-continuity methods; 3. Method of integral relations and polynomial approximation; 4. Relaxation techniques and the unsteady approach method; 5. The inverse problem; 6. Procedures with nonequilibrium; CHAPTER VII - OTHER METHODS FOR LOCALLY SUPERSONIC FLOWS; 1. Method of characteristics; 2. Shock-expansion theory; 3. Tangent-wedge and tangent-cone; 4. Conical flows; 5. Nonequilibrium flows; CITED REFERENCES; SYMBOL INDEX; SUBSCRIPTS; SUPERSCRIPTS MATHEMATICAL AND SPECIAL SYMBOLSAUTHOR INDEX |
| Record Nr. | UNINA-9911006632203321 |
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Hayes Wallace D
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| Newburyport, : Dover Publications, 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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