[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], nach der Bestellung gedruckt Neuware - The recent advances in aerospace vehicle technology demands the best possible … Mehr…
[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], nach der Bestellung gedruckt Neuware - The recent advances in aerospace vehicle technology demands the best possible propulsive balance to provide better thrust and minimum drag. Air-breathing engines are the best choice for the propulsion due to its minimum weight. The efficiency of such engines depend upon the quality of air entering for combustion. This book provides complete flow analysis of both pure inline-compression and mixed-compression inlets. Two dimensional simulations were carried out with SST k- model using FLUENT. The boundary layer formed inner side of the engine had an adverse pressure gradient on the ramp producing a boundary layer separation. Due to this the boundary layer thickens and the static pressure starts to decrease whose effect leads till the trailing edge of inlet. Small wedge shaped Micro-Vortex Generator (MVG) inside the inlet smoothen the generated shock-boundary layers and thereby an efficient compression is obtained . The analysis should help shed some light on hypersonic inlet design optimization at off-design condition and should be especially useful to researchers and academicians in the field of Aerospace Engineering. 100 pp. Englisch, Books<
[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], nach der Bestellung gedruckt Neuware -The recent advances in aerospace vehicle technology demands the best possible p… Mehr…
[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], nach der Bestellung gedruckt Neuware -The recent advances in aerospace vehicle technology demands the best possible propulsive balance to provide better thrust and minimum drag. Air-breathing engines are the best choice for the propulsion due to its minimum weight. The efficiency of such engines depend upon the quality of air entering for combustion. This book provides complete flow analysis of both pure inline-compression and mixed-compression inlets. Two dimensional simulations were carried out with SST k- model using FLUENT. The boundary layer formed inner side of the engine had an adverse pressure gradient on the ramp producing a boundary layer separation. Due to this the boundary layer thickens and the static pressure starts to decrease whose effect leads till the trailing edge of inlet. Small wedge shaped Micro-Vortex Generator (MVG) inside the inlet smoothen the generated shock-boundary layers and thereby an efficient compression is obtained . The analysis should help shed some light on hypersonic inlet design optimization at off-design condition and should be especially useful to researchers and academicians in the field of Aerospace Engineering. 100 pp. Englisch, Books<
Paperback, [PU: LAP Lambert Academic Publishing], The recent advances in aerospace vehicle technology demands the best possible propulsive balance to provide better thrust and minimum dra… Mehr…
Paperback, [PU: LAP Lambert Academic Publishing], The recent advances in aerospace vehicle technology demands the best possible propulsive balance to provide better thrust and minimum drag. Air-breathing engines are the best choice for the propulsion due to its minimum weight. The efficiency of such engines depend upon the quality of air entering for combustion. This book provides complete flow analysis of both pure inline-compression and mixed-compression inlets. Two dimensional simulations were carried out with SST k-ω model using FLUENT. The boundary layer formed inner side of the engine had an adverse pressure gradient on the ramp producing a boundary layer separation. Due to this the boundary layer thickens and the static pressure starts to decrease whose effect leads till the trailing edge of inlet. Small wedge shaped Micro-Vortex Generator (MVG) inside the inlet smoothen the generated shock-boundary layers and thereby an efficient compression is obtained . The analysis should help shed some light on hypersonic inlet design optimization at off-design condition and should be especially useful to researchers and academicians in the field of Aerospace Engineering., Aerospace & Aviation Technology<
[ED: Kartoniert / Broschiert], [PU: LAP LAMBERT Academic Publishing], Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: V. Ku… Mehr…
[ED: Kartoniert / Broschiert], [PU: LAP LAMBERT Academic Publishing], Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: V. Kumar VivekCompleted Masters in Aeronautical Engineering(Aerodynamics) from Hindustan Institute of Technology & Science, Chennai and undergrad, DE, [SC: 0.00], Neuware, gewerbliches Angebot, Hardcover, 100, [GW: 159g], 1. Auflage, Banküberweisung, PayPal, [CT: Naturwissenschaft/Mathematik / Sonstiges - Naturwissenschaften]<
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[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], TECHNIK LUFTFAHRTTECHNIK RAUMFAHRTTECHNIK LUFTFAHRZEUGE, Dieser Artikel ist ein Print on Demand Artikel und wird nach… Mehr…
[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], TECHNIK LUFTFAHRTTECHNIK RAUMFAHRTTECHNIK LUFTFAHRZEUGE, Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung für Sie gedruckt. The recent advances in aerospace vehicle technology demands the best possible propulsive balance to provide better thrust and minimum drag. Air-breathing engine, Books<
[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], nach der Bestellung gedruckt Neuware - The recent advances in aerospace vehicle technology demands the best possible … Mehr…
[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], nach der Bestellung gedruckt Neuware - The recent advances in aerospace vehicle technology demands the best possible propulsive balance to provide better thrust and minimum drag. Air-breathing engines are the best choice for the propulsion due to its minimum weight. The efficiency of such engines depend upon the quality of air entering for combustion. This book provides complete flow analysis of both pure inline-compression and mixed-compression inlets. Two dimensional simulations were carried out with SST k- model using FLUENT. The boundary layer formed inner side of the engine had an adverse pressure gradient on the ramp producing a boundary layer separation. Due to this the boundary layer thickens and the static pressure starts to decrease whose effect leads till the trailing edge of inlet. Small wedge shaped Micro-Vortex Generator (MVG) inside the inlet smoothen the generated shock-boundary layers and thereby an efficient compression is obtained . The analysis should help shed some light on hypersonic inlet design optimization at off-design condition and should be especially useful to researchers and academicians in the field of Aerospace Engineering. 100 pp. Englisch, Books<
[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], nach der Bestellung gedruckt Neuware -The recent advances in aerospace vehicle technology demands the best possible p… Mehr…
[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], nach der Bestellung gedruckt Neuware -The recent advances in aerospace vehicle technology demands the best possible propulsive balance to provide better thrust and minimum drag. Air-breathing engines are the best choice for the propulsion due to its minimum weight. The efficiency of such engines depend upon the quality of air entering for combustion. This book provides complete flow analysis of both pure inline-compression and mixed-compression inlets. Two dimensional simulations were carried out with SST k- model using FLUENT. The boundary layer formed inner side of the engine had an adverse pressure gradient on the ramp producing a boundary layer separation. Due to this the boundary layer thickens and the static pressure starts to decrease whose effect leads till the trailing edge of inlet. Small wedge shaped Micro-Vortex Generator (MVG) inside the inlet smoothen the generated shock-boundary layers and thereby an efficient compression is obtained . The analysis should help shed some light on hypersonic inlet design optimization at off-design condition and should be especially useful to researchers and academicians in the field of Aerospace Engineering. 100 pp. Englisch, Books<
Paperback, [PU: LAP Lambert Academic Publishing], The recent advances in aerospace vehicle technology demands the best possible propulsive balance to provide better thrust and minimum dra… Mehr…
Paperback, [PU: LAP Lambert Academic Publishing], The recent advances in aerospace vehicle technology demands the best possible propulsive balance to provide better thrust and minimum drag. Air-breathing engines are the best choice for the propulsion due to its minimum weight. The efficiency of such engines depend upon the quality of air entering for combustion. This book provides complete flow analysis of both pure inline-compression and mixed-compression inlets. Two dimensional simulations were carried out with SST k-ω model using FLUENT. The boundary layer formed inner side of the engine had an adverse pressure gradient on the ramp producing a boundary layer separation. Due to this the boundary layer thickens and the static pressure starts to decrease whose effect leads till the trailing edge of inlet. Small wedge shaped Micro-Vortex Generator (MVG) inside the inlet smoothen the generated shock-boundary layers and thereby an efficient compression is obtained . The analysis should help shed some light on hypersonic inlet design optimization at off-design condition and should be especially useful to researchers and academicians in the field of Aerospace Engineering., Aerospace & Aviation Technology<
[ED: Kartoniert / Broschiert], [PU: LAP LAMBERT Academic Publishing], Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: V. Ku… Mehr…
[ED: Kartoniert / Broschiert], [PU: LAP LAMBERT Academic Publishing], Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: V. Kumar VivekCompleted Masters in Aeronautical Engineering(Aerodynamics) from Hindustan Institute of Technology & Science, Chennai and undergrad, DE, [SC: 0.00], Neuware, gewerbliches Angebot, Hardcover, 100, [GW: 159g], 1. Auflage, Banküberweisung, PayPal, [CT: Naturwissenschaft/Mathematik / Sonstiges - Naturwissenschaften]<
Versandkosten:Versandkostenfrei, Versand nach Deutschland. (EUR 0.00) Moluna GmbH
[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], TECHNIK LUFTFAHRTTECHNIK RAUMFAHRTTECHNIK LUFTFAHRZEUGE, Dieser Artikel ist ein Print on Demand Artikel und wird nach… Mehr…
[EAN: 9783659158346], Neubuch, [PU: LAP Lambert Academic Publishing], TECHNIK LUFTFAHRTTECHNIK RAUMFAHRTTECHNIK LUFTFAHRZEUGE, Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung für Sie gedruckt. The recent advances in aerospace vehicle technology demands the best possible propulsive balance to provide better thrust and minimum drag. Air-breathing engine, Books<
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Detailangaben zum Buch - Effect Of Micro-vortex Generator In Hypersonic Inlet
EAN (ISBN-13): 9783659158346 ISBN (ISBN-10): 3659158348 Gebundene Ausgabe Taschenbuch Erscheinungsjahr: 2012 Herausgeber: Lap Lambert Academic Publishing Jun 2012
Buch in der Datenbank seit 2008-03-28T18:01:15+01:00 (Berlin) Detailseite zuletzt geändert am 2023-10-29T09:24:12+01:00 (Berlin) ISBN/EAN: 3659158348
ISBN - alternative Schreibweisen: 3-659-15834-8, 978-3-659-15834-6 Alternative Schreibweisen und verwandte Suchbegriffe: Titel des Buches: fluid vortices, micro, cfd, computational dynamics, vortex dynamics, generator
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