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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 [[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-9910827022103321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, c2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Analysis of nonequilibrium air streams in the Ames 1-foot shock tunnel / / by Robert S. Hiers, Jr., and John O. Reller, Jr
| Analysis of nonequilibrium air streams in the Ames 1-foot shock tunnel / / by Robert S. Hiers, Jr., and John O. Reller, Jr |
| Autore | Hiers Robert S. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 |
| Descrizione fisica | 1 online resource (25 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Air flow
Aerodynamics Shock tunnels Nonequilibrium thermodynamics Aerodynamics, Hypersonic Air flow - Measurement |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716071503321 |
Hiers Robert S.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Analytical and experimental studies of shock interference heating in hypersonic flows / / by J. Wayne Keyes and Frank D. Hains
| Analytical and experimental studies of shock interference heating in hypersonic flows / / by J. Wayne Keyes and Frank D. Hains |
| Autore | Keyes J. Wayne |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , May 1973 |
| Descrizione fisica | 1 online resource (iv, 137 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Fluid mechanics
Shock waves Aerodynamic heating Aerodynamics, Hypersonic Boundary layer |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716562003321 |
|
Keyes J. Wayne
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| Washington, D.C. : , : National Aeronautics and Space Administration, , May 1973 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8 / / by P. Calvin Stainback
| Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8 / / by P. Calvin Stainback |
| Autore | Stainback P. Calvin |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 |
| Descrizione fisica | 1 online resource (76 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Reynolds number
Aerodynamics Mach number Aerodynamics, Hypersonic Angle of attack (Aerodynamics) Noses (Space vehicles) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716080803321 |
|
Stainback P. Calvin
|
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| Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Experimental study of nozzle wall boundary layers at Mach numbers 20 to 47 / / by Joseph H. Kemp and F. Kevin Owen
| Experimental study of nozzle wall boundary layers at Mach numbers 20 to 47 / / by Joseph H. Kemp and F. Kevin Owen |
| Autore | Kemp Joseph H. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1972 |
| Descrizione fisica | 1 online resource (vii, 101 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Jet nozzles
Turbulent boundary layer Wall pressure Wall pressure (Aerodynamics) Aerodynamics, Hypersonic |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716571203321 |
|
Kemp Joseph H.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , October 1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Flow-field investigations on the X-15 airplane and model up to hypersonic speeds / / by L.J. McLain and Murray Palitz
| Flow-field investigations on the X-15 airplane and model up to hypersonic speeds / / by L.J. McLain and Murray Palitz |
| Autore | McLain L. J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , September 1968 |
| Descrizione fisica | 1 online resource (31 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
X-15 (Rocket aircraft)
Aerodynamics, Hypersonic |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714058003321 |
|
McLain L. J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , September 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Forces due to air and helium jets impinging normal to a flat plate for near-vacuum and sea-level ambient pressures / / by Sherwood Hoffman and Joseph J. Janos
| Forces due to air and helium jets impinging normal to a flat plate for near-vacuum and sea-level ambient pressures / / by Sherwood Hoffman and Joseph J. Janos |
| Autore | Hoffman Sherwood |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , January 1971 |
| Descrizione fisica | 1 online resource (22 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Hypersonic aircraft
Aerodynamics, Hypersonic Helium Nozzles Dead loads (Mechanics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716001903321 |
|
Hoffman Sherwood
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| Washington, D.C. : , : National Aeronautics and Space Administration, , January 1971 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Heat-transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7 / / by Irving Weinstein
| Heat-transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7 / / by Irving Weinstein |
| Autore | Weinstein Irving |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , January 1973 |
| Descrizione fisica | 1 online resource (38 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Cylinders
Aerodynamic loads Combustion products Aerodynamic heating Heat - Transmission Aerodynamics, Hypersonic Aerodynamic load |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716581203321 |
|
Weinstein Irving
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| Washington, D.C. : , : National Aeronautics and Space Administration, , January 1973 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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