Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724372925
Category :
Languages : en
Pages : 242
Book Description
Reports by the staff of the University of Queensland on various research studies related to the advancement of scramjet technology are presented. These reports document the tests conducted in the reflected shock tunnel T4 and supporting research facilities that have been used to study the injection, mixing, and combustion of hydrogen fuel in generic scramjets at flow conditions typical of hypersonic flight. In addition, topics include the development of instrumentation and measurement technology, such as combustor wall shear and stream composition in pulse facilities, and numerical studies and analyses of the scramjet combustor process and the test facility operation. Wendt, M. and Nettleton, M. and Morgan, R. G. and Skinner, K. and Casey, R. and Stalker, R. and Brescianini, C. and Paull, A. and Allen, G. and Smart, M. Unspecified Center NASA-CR-191428, NAS 1.26:191428 NAGW-674; RTOP 505-70-62-02...
Shock Tunnel Studies of Scramjet Phenomena, Supplement 6
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724372925
Category :
Languages : en
Pages : 242
Book Description
Reports by the staff of the University of Queensland on various research studies related to the advancement of scramjet technology are presented. These reports document the tests conducted in the reflected shock tunnel T4 and supporting research facilities that have been used to study the injection, mixing, and combustion of hydrogen fuel in generic scramjets at flow conditions typical of hypersonic flight. In addition, topics include the development of instrumentation and measurement technology, such as combustor wall shear and stream composition in pulse facilities, and numerical studies and analyses of the scramjet combustor process and the test facility operation. Wendt, M. and Nettleton, M. and Morgan, R. G. and Skinner, K. and Casey, R. and Stalker, R. and Brescianini, C. and Paull, A. and Allen, G. and Smart, M. Unspecified Center NASA-CR-191428, NAS 1.26:191428 NAGW-674; RTOP 505-70-62-02...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724372925
Category :
Languages : en
Pages : 242
Book Description
Reports by the staff of the University of Queensland on various research studies related to the advancement of scramjet technology are presented. These reports document the tests conducted in the reflected shock tunnel T4 and supporting research facilities that have been used to study the injection, mixing, and combustion of hydrogen fuel in generic scramjets at flow conditions typical of hypersonic flight. In addition, topics include the development of instrumentation and measurement technology, such as combustor wall shear and stream composition in pulse facilities, and numerical studies and analyses of the scramjet combustor process and the test facility operation. Wendt, M. and Nettleton, M. and Morgan, R. G. and Skinner, K. and Casey, R. and Stalker, R. and Brescianini, C. and Paull, A. and Allen, G. and Smart, M. Unspecified Center NASA-CR-191428, NAS 1.26:191428 NAGW-674; RTOP 505-70-62-02...
Shock Tunnel Studies of Scramjet Phenomena, Supplement 6
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 244
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 244
Book Description
Shock Tunnel Studies of Scramjet Phenomena, Supplement 5
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724372802
Category :
Languages : en
Pages : 202
Book Description
A series of reports are presented on SCRAMjet studies, shock tunnel studies, and expansion tube studies. The SCRAMjet studies include: (1) Investigation of a Supersonic Combustion Layer; (2) Wall Injected SCRAMjet Experiments; (3) Supersonic Combustion with Transvers, Circular, Wall Jets; (4) Dissociated Test Gas Effects on SCRAMjet Combustors; (5) Use of Silane as a Fuel Additive for Hypersonic Thrust Production, (6) Pressure-length Correlations in Supersonic Combustion; (7) Hot Hydrogen Injection Technique for Shock Tunnels; (8) Heat Release - Wave Interaction Phenomena in Hypersonic Flows; (9) A Study of the Wave Drag in Hypersonic SCRAMjets; (10) Parametric Study of Thrust Production in the Two Dimensional SCRAMjet; (11) The Design of a Mass Spectrometer for use in Hypersonic Impulse Facilities; and (12) Development of a Skin Friction Gauge for use in an Impulse Facility. The shock tunnel studies include: (1) Hypervelocity flow in Axisymmetric Nozzles; (2) Shock Tunnel Development; and (3) Real Gas Efects in Hypervelocity Flows over an Inclined Cone. The expansion tube studies include: (1) Investigation of Flow Characteristics in TQ Expansion Tube; and (2) Disturbances in the Driver Gas of a Shock Tube. Casey, R. and Stalker, R. J. and Brescianini, C. P. and Morgan, R. G. and Jacobs, P. A. and Wendt, M. and Ward, N. R. and Akman, N. and Allen, G. A. and Skinner, K. Unspecified Center NASA-CR-182096-SUPPL-5, NAS 1.26:182096-SUPPL-5 NAGW-674; RTOP 505-62-40-02...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724372802
Category :
Languages : en
Pages : 202
Book Description
A series of reports are presented on SCRAMjet studies, shock tunnel studies, and expansion tube studies. The SCRAMjet studies include: (1) Investigation of a Supersonic Combustion Layer; (2) Wall Injected SCRAMjet Experiments; (3) Supersonic Combustion with Transvers, Circular, Wall Jets; (4) Dissociated Test Gas Effects on SCRAMjet Combustors; (5) Use of Silane as a Fuel Additive for Hypersonic Thrust Production, (6) Pressure-length Correlations in Supersonic Combustion; (7) Hot Hydrogen Injection Technique for Shock Tunnels; (8) Heat Release - Wave Interaction Phenomena in Hypersonic Flows; (9) A Study of the Wave Drag in Hypersonic SCRAMjets; (10) Parametric Study of Thrust Production in the Two Dimensional SCRAMjet; (11) The Design of a Mass Spectrometer for use in Hypersonic Impulse Facilities; and (12) Development of a Skin Friction Gauge for use in an Impulse Facility. The shock tunnel studies include: (1) Hypervelocity flow in Axisymmetric Nozzles; (2) Shock Tunnel Development; and (3) Real Gas Efects in Hypervelocity Flows over an Inclined Cone. The expansion tube studies include: (1) Investigation of Flow Characteristics in TQ Expansion Tube; and (2) Disturbances in the Driver Gas of a Shock Tube. Casey, R. and Stalker, R. J. and Brescianini, C. P. and Morgan, R. G. and Jacobs, P. A. and Wendt, M. and Ward, N. R. and Akman, N. and Allen, G. A. and Skinner, K. Unspecified Center NASA-CR-182096-SUPPL-5, NAS 1.26:182096-SUPPL-5 NAGW-674; RTOP 505-62-40-02...
Shock Tunnel Studies of Scramjet Phenomena, Supplement 7
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 152
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 152
Book Description
Shock Tunnel Studies of Scramjet Phenomena, Supplement 8
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 138
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 138
Book Description
Shock Tunnel Studies of Scramjet Phenomena, Supplement 5
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 204
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 204
Book Description
Further Shock Tunnel Studies of Scramjet Phenomena
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :
Book Description
Scramjet Propulsion
Author: E. T. Curran
Publisher: AIAA
ISBN: 9781600864414
Category : Airplanes
Languages : en
Pages : 1354
Book Description
Publisher: AIAA
ISBN: 9781600864414
Category : Airplanes
Languages : en
Pages : 1354
Book Description
Shock Tunnel Studies of Scramjet Phenomena 1995
Author: R. G. Morgan
Publisher:
ISBN:
Category :
Languages : en
Pages : 108
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 108
Book Description
Further Shock Tunnel Studies of Scramjet Phenomena
Author: R. G. Morgan
Publisher:
ISBN:
Category :
Languages : en
Pages : 57
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 57
Book Description