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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 | ||
| ||
Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° / / by Jim A. Penland
| Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° / / by Jim A. Penland |
| Autore | Penland Jim A. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1957 |
| Descrizione fisica | 1 online resource (32 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Cylinders - Aerodynamics
Aerodynamic load Wind tunnel testing Hypersonic wind tunnels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to ninety degrees |
| Record Nr. | UNINA-9910713872803321 |
Penland Jim A.
|
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1957 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Calibration of Lewis hypersonic tunnel facility at Mach 5, 6, and 7 / / by Richard R. Cullom and Erwin A. Lezberg
| Calibration of Lewis hypersonic tunnel facility at Mach 5, 6, and 7 / / by Richard R. Cullom and Erwin A. Lezberg |
| Autore | Cullom Richard R. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , November 1972 |
| Descrizione fisica | 1 online resource (30 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Hypersonic wind tunnels
Wind tunnels Hypersonic wind tunnels - Calibration |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716530003321 |
|
Cullom Richard R.
|
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| Washington, D.C. : , : National Aeronautics and Space Administration, , November 1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 / / Brian R. Hollis
| Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 / / Brian R. Hollis |
| Autore | Hollis Brian R (Brian Ray) |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2017 |
| Descrizione fisica | 1 online resource (viii, 168 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Boundary layer transition
Hypersonic wind tunnels Surface roughness Surface roughness effects Thermography |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705705303321 |
|
Hollis Brian R (Brian Ray)
|
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Langley 8-ft. HTT Test 139 gas analyses / / Danny R. Sprinkle and Patricia P. Davis
| Langley 8-ft. HTT Test 139 gas analyses / / Danny R. Sprinkle and Patricia P. Davis |
| Autore | Sprinkle Danny R. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 1999 |
| Descrizione fisica | 1 online resource (190 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Gas analysis
Wind tunnel calibration Mass spectroscopy Hypersonic wind tunnels Blowdown wind tunnels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706119303321 |
|
Sprinkle Danny R.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF / / H. Douglas Perkins, Scott R. Thomas, and William D. Pack
| Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF / / H. Douglas Perkins, Scott R. Thomas, and William D. Pack |
| Autore | Perkins H. Douglas |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996 |
| Descrizione fisica | 1 online resource (13 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Flexibility
Engine tests Hypersonic speed Hypersonic wind tunnels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Mach five to seven rocket based combined cycle propulsion system testing at NASA Lewis Research Center hypersonic tunnel facility |
| Record Nr. | UNINA-9910707307103321 |
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Perkins H. Douglas
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , December 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
The mothball, sustainment, and proposed reactivation of the hypersonic tunnel facility (HTF) at NASA Glenn Research Center Plum Brook Station / / Scott R. Thomas [and four others]
| The mothball, sustainment, and proposed reactivation of the hypersonic tunnel facility (HTF) at NASA Glenn Research Center Plum Brook Station / / Scott R. Thomas [and four others] |
| Autore | Thomas Scott R (Engineer) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2010 |
| Descrizione fisica | 1 online resource (14 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Hypersonic wind tunnels
Test facilities Hypersonic flight Hypersonic speed Propulsion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Mothball, sustainment, and proposed reactivation of the hypersonic tunnel facility |
| Record Nr. | UNINA-9910700981503321 |
|
Thomas Scott R (Engineer)
|
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2010 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Quantitative global heat transfer in a Mach-6 quiet tunnel / / John P. Sullivan [and ten others]
| Quantitative global heat transfer in a Mach-6 quiet tunnel / / John P. Sullivan [and ten others] |
| Autore | Sullivan John P. |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (148 pages) : color illustrations |
| Collana | [NASA contractor report] |
| Soggetto topico |
Heat transfer
Hypersonic speed Temperature sensitive paints Wind tunnel tests Hypersonic wind tunnels Heat flux Mathematical models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702091603321 |
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Sullivan John P.
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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