FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W964093386> ?p ?o ?g. }

• W964093386 abstract "One of the major technological innovations that are necessary for faster and cheaper access-to-space will be the commercial realization of supersonic combustion jet engines (SCRAMJET). The establishment of the flow through the inlet is one the prime requirement for the success of a SCRAMJET engine. The flow through a SCRAMJET inlet is dominated by inviscid /viscous coupling, transition, shock-shock interaction, shock boundary layer interaction, blunt leading edge effects and flow profile effects. Although the literature is exhaustive on various aspects of flow features associated with SCRAMJET engines, very little is known on the fundamental gasdynamic features dictating the flow establishment in the SCRAMJET inlet. On one hand we need the reduction of flight Mach number to manageable supersonic values inside the SCRAMJET combustor, but on the other hand we have to achieve this with minimum total pressure loss. Hence the dynamics of ramp/cowl shock interaction process ahead of the inlet has a direct bearing on the quality and type of flow inside the SCRAMJET engine. There is virtually no data base in the open literature focusing specifically on the cowl/ramp shock interactions at hypersonic Mach numbers. Hence in this backdrop, the main aim of the present investigation is to systematically understand the ramp/cowl shock interaction processes in front of a generic inlet model. Since we are primarily concerned with the shock interaction process ahead of the cowl all the investigations are carried out without any fuel injection. Variable geometry is necessary if we want to operate the inlet for a wide range of Mach numbers in actual flight. The investigation mainly comprises of three variable geometry configurations; namely, variation of contraction ratios at 00 cowl (CR 8.4, 5.0 and 4.3), variation of cowl length for a given chamber height (four lengths of cowls at 10 mm chamber height) and variation of cowl angle (three angles cowl each for two chamber heights). The change in cowl configuration results in different ramp/cowl shock interaction processes affecting the performance of the inlet. Experiments are performed in IISc hypersonic shock tunnel HST 2 (test time ~ 1 ms) at two nominal Mach numbers 8.0 and 5.74 for design and off-design testing conditions. Exhaustive numerical simulations are also performed to compliment the experiments. Further the effect of concentrated energy deposition on forebody /cowl shock interactions has also been investigated. A 2D, planar, single ramp scramjet inlet model has been designed and fabricated along with various cowl geometries and tested in a hypersonic shock tunnel to characterize the forebody/cowl shock interaction process for different inlet configurations. Further a DC plasma power unit and a plasma torch have been designed, developed and fabricated to serve as energy source for conducting flow-alteration experiments in the inlet model. The V-I characteristics of the plasma torch is studied and an estimation of plasma temperature is also performed as a part of…" @default.
• W964093386 created "2016-06-24" @default.
• W964093386 creator A5067722754 @default.
• W964093386 date "2010-08-05" @default.
• W964093386 modified "2023-09-23" @default.
• W964093386 title "Investigation Of Ramp/Cowl Shock Interaction Processes Near A Generic Scramjet Inlet At Hypersonic Mach Number" @default.
• W964093386 hasPublicationYear "2010" @default.
• W964093386 type Work @default.
• W964093386 sameAs 964093386 @default.
• W964093386 citedByCount "0" @default.
• W964093386 crossrefType "dissertation" @default.
• W964093386 hasAuthorship W964093386A5067722754 @default.
• W964093386 hasConcept C105923489 @default.
• W964093386 hasConcept C116575374 @default.
• W964093386 hasConcept C121332964 @default.
• W964093386 hasConcept C122824865 @default.
• W964093386 hasConcept C126322002 @default.
• W964093386 hasConcept C127413603 @default.
• W964093386 hasConcept C146978453 @default.
• W964093386 hasConcept C165231844 @default.
• W964093386 hasConcept C178790620 @default.
• W964093386 hasConcept C185592680 @default.
• W964093386 hasConcept C205991772 @default.
• W964093386 hasConcept C2781300812 @default.
• W964093386 hasConcept C56278489 @default.
• W964093386 hasConcept C57879066 @default.
• W964093386 hasConcept C71924100 @default.
• W964093386 hasConcept C83104080 @default.
• W964093386 hasConceptScore W964093386C105923489 @default.
• W964093386 hasConceptScore W964093386C116575374 @default.
• W964093386 hasConceptScore W964093386C121332964 @default.
• W964093386 hasConceptScore W964093386C122824865 @default.
• W964093386 hasConceptScore W964093386C126322002 @default.
• W964093386 hasConceptScore W964093386C127413603 @default.
• W964093386 hasConceptScore W964093386C146978453 @default.
• W964093386 hasConceptScore W964093386C165231844 @default.
• W964093386 hasConceptScore W964093386C178790620 @default.
• W964093386 hasConceptScore W964093386C185592680 @default.
• W964093386 hasConceptScore W964093386C205991772 @default.
• W964093386 hasConceptScore W964093386C2781300812 @default.
• W964093386 hasConceptScore W964093386C56278489 @default.
• W964093386 hasConceptScore W964093386C57879066 @default.
• W964093386 hasConceptScore W964093386C71924100 @default.
• W964093386 hasConceptScore W964093386C83104080 @default.
• W964093386 hasLocation W9640933861 @default.
• W964093386 hasOpenAccess W964093386 @default.
• W964093386 hasPrimaryLocation W9640933861 @default.
• W964093386 hasRelatedWork W1773751526 @default.
• W964093386 hasRelatedWork W1989082349 @default.
• W964093386 hasRelatedWork W2009254629 @default.
• W964093386 hasRelatedWork W2021392710 @default.
• W964093386 hasRelatedWork W2026085013 @default.
• W964093386 hasRelatedWork W2038438427 @default.
• W964093386 hasRelatedWork W2049345614 @default.
• W964093386 hasRelatedWork W2109460660 @default.
• W964093386 hasRelatedWork W2162902640 @default.
• W964093386 hasRelatedWork W2166938102 @default.
• W964093386 hasRelatedWork W2254580458 @default.
• W964093386 hasRelatedWork W2312888283 @default.
• W964093386 hasRelatedWork W2321066747 @default.
• W964093386 hasRelatedWork W2324967786 @default.
• W964093386 hasRelatedWork W2357781514 @default.
• W964093386 hasRelatedWork W2915610531 @default.
• W964093386 hasRelatedWork W2941735003 @default.
• W964093386 hasRelatedWork W2985190667 @default.
• W964093386 hasRelatedWork W656735213 @default.
• W964093386 hasRelatedWork W791269599 @default.
• W964093386 isParatext "false" @default.
• W964093386 isRetracted "false" @default.
• W964093386 magId "964093386" @default.
• W964093386 workType "dissertation" @default.