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| 050 |
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4 |
|a TL709.3.S37
|b S37 2000eb
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| 049 |
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|a HCDD
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| 245 |
0 |
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|a Scramjet propulsion /
|c edited by E.T. Curran, S.N.B. Murthy.
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| 260 |
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|a Reston, Va. :
|b American Institute of Aeronautics and Astronautics,
|c ©2000.
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| 300 |
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|a 1 online resource (xxvii, 1293 pages) :
|b illustrations
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| 336 |
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|a text
|b txt
|2 rdacontent
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| 337 |
|
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|a computer
|b c
|2 rdamedia
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| 338 |
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|a online resource
|b cr
|2 rdacarrier
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| 490 |
1 |
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|a Progress in astronautics and aeronautics ;
|v v. 189
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| 504 |
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|a Includes bibliographical references.
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| 505 |
0 |
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|a Cover -- Title -- Copyright -- Contents -- Preface -- Introduction -- I. International Efforts -- II. Inlets, Combustors, and Fuels -- III. Overall Systems -- IV. Future Developments -- V. Closing Comments -- References -- Chapter 1 Scramjet Testing in the T3 and T4 Hypersonic Impulse Facilities -- Nomenclature -- I. History, Aims, and Developments -- II. Facility and Instrumentation -- III. Fuel-Injection Systems -- A. Wall-Injection Combustion Results -- B. Wall-Injection Film-Cooling Results -- C. Port-Injection Results -- D. Central Injection -- IV. Combustion/Mixing Processes.
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| 505 |
8 |
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|a A. Mixing Controlled Combustion -- B. Kinetically Controlled Combustion -- C. Shock-Induced Ignition -- D. Shock-Induced Mixing -- V. Simple Theoretical Combustor and Thrust Model -- VI. Experimental Results of Specific Impulse -- VII. Effects of Atomic Oxygen and Nitric Oxide in the Freestream -- VIII. Different Fuels -- A. Hydrocarbon Fuels -- B. Silane-Enriched Fuels -- IX. Integrated Scramjet Measurements -- X. Skin-Friction Measurements -- XI. Discussion and Review -- Acknowledgments -- Bibliography -- Chapter 2 Scramjet Developments in France -- I. Historical Overview.
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| 505 |
8 |
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|a II. Basic Research on Diffusion Flame Combustion (1962-1967) -- A. Combustion in a Cylindrical Duct -- B. Freejet Test -- C. Combustion in a Divergent Duct -- D. Synthesis -- III. ESOPE Program (1966-1973) -- A. Origin and Principal Aims -- B. Studies Results -- C. Synthesis -- IV. Studies on Shock-Induced Combustion -- A. Principle -- B. ENSMA and LATECAM Studies -- V. Prepha Program (1992-1997) -- A. Origin and Principal Aims -- B. System Studies -- C. Development of New Test Facilities -- D. Numerical Means -- E. Development of Scramjet Components -- Color Plates.
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| 505 |
8 |
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|a F. Materials and Cooled Structures -- G. Flight Testing -- VI. Perspectives -- A. Space Application -- B. Missile Application -- References -- Chapter 3 Scramjet Investigations Within the German Hypersonics Technology Program (1993-1996) -- I. German Hypersonics Technology Program and Scramjet-Related Activities -- A. German Hypersonics Technology Program -- B. Scramjet Related Activities Within the HTP -- II. Theoretical Investigations for Scramjet Intake Designs -- A. Activities at Dasa-MT633 -- B. Activities at RWTH Aachen.
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| 505 |
8 |
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|a III. Theoretical and Experimental Investigations of Scramjet Combustion at TsAGI and DLR Lampoldshausen -- A. Combustor Model Design -- B. Fuel-Injection Modules -- C. Test Results -- IV. Freejet Wind-tunnel Testing of Scramjet Propulsion Systems at TsAGI -- A. Scramjet Propulsion System Model Concept -- B. Testing Focus -- C. Test Results -- V. Considerations for Flight Testing Small-Scale Scramjet Modules Using the RADUGA-D2 Flying Testbed -- A. Objectives for Flight Testing -- B. RADUGA-D2 Flying Testbed -- C. Flight Test Trajectory and Integration of Scramjet in the RADUGA-D2 -- References.
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| 650 |
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|a Airplanes
|x Scramjet engines.
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| 650 |
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|a Jet propulsion.
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| 650 |
|
7 |
|a Airplanes
|x Scramjet engines
|2 fast
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| 650 |
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7 |
|a Jet propulsion
|2 fast
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| 655 |
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7 |
|a dissertations.
|2 aat
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| 655 |
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7 |
|a Academic theses
|2 fast
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| 655 |
|
7 |
|a Academic theses.
|2 lcgft
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| 655 |
|
7 |
|a Thèses et écrits académiques.
|2 rvmgf
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| 700 |
1 |
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|a Curran, E. T.
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| 700 |
1 |
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|a Murthy, S. N. B.
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| 758 |
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|i has work:
|a Scramjet propulsion (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCXVTTMxFhVpT6VTcgXbDFX
|4 https://id.oclc.org/worldcat/ontology/hasWork
|
| 776 |
0 |
8 |
|i Print version:
|t Scramjet propulsion.
|d Reston, Va. : American Institute of Aeronautics and Astronautics, ©2000
|w (DLC) 2002277315
|
| 830 |
|
0 |
|a Progress in astronautics and aeronautics ;
|v v. 189.
|
| 856 |
4 |
0 |
|u https://ebookcentral.proquest.com/lib/holycrosscollege-ebooks/detail.action?docID=3111567
|y Click for online access
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| 903 |
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|a EBC-AC
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| 994 |
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|a 92
|b HCD
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