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dc.contributor.authorFerrar, Anthony Mauriceen_US
dc.date.accessioned2014-03-14T20:50:40Z
dc.date.available2014-03-14T20:50:40Z
dc.date.issued2011-12-15en_US
dc.identifier.otheretd-12222011-143750en_US
dc.identifier.urihttp://hdl.handle.net/10919/36408
dc.description.abstractHighly integrated airframe-propulsion systems featuring ingestion of the airframe boundary layer oer reduced noise, emissions, and fuel consumption. Embedded engine systems are envisioned which require boundary layer ingesting (BLI) serpentine inlets to provide the needed air ow to the engine. These inlets produce distorted ow proles that can cause aeromechanical, stability, and performance changes in embedded engines. Proper design of embedded engine systems requires understanding of the underlying uid dynamics that occur within serpentine inlets. A serpentine inlet was tested in a specially designed wind tunnel that simulated boundary layer ingestion in a full-scale realistic environment. The measured total pressure proles at the inlet and exit planes of the duct, and the static pressure distributions along the walls provided useful data related to the ow in BLI serpentine inlet systems. A bleed ow control system was tested that utilized no more than 2% of the total inlet ow. Two bleed slots were employed, one near the rst bend of the S-duct and one near second. The bleed system successfully reduced inlet distortions by as much as 30%, implying improvements in stall margin and engine performance. Analysis of the wake shape entering the S-duct showed that the airframe and inlet duct are both important components of a wake-ingesting inlet/diusion system. Shape eects and static pressure distributions determined ow transport within the serpentine inlet. Flow separation within the S-duct increased distortion at the engine inlet plane. Discussion of airframe/inlet/engine compatibility demonstrates that embedded engine systems require multi-disciplinary collaborative design eorts. An included fundamental analysis provides performance estimates and design guidelines. The ideal airframe performance improvement associated with wake-ingestion is estimated.en_US
dc.publisherVirginia Techen_US
dc.relation.haspartFerrar_AM_T_2011.pdfen_US
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subjectboundary layer ingestionen_US
dc.subjectwake ingestionen_US
dc.subjectdistortionen_US
dc.subjectflow controlen_US
dc.subjectdiffuseren_US
dc.subjectinleten_US
dc.titleMeasurements of Flow in Boundary Layer Ingesting Serpentine Inletsen_US
dc.typeThesisen_US
dc.contributor.departmentMechanical Engineeringen_US
dc.description.degreeMaster of Scienceen_US
thesis.degree.nameMaster of Scienceen_US
thesis.degree.levelmastersen_US
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen_US
thesis.degree.disciplineMechanical Engineeringen_US
dc.contributor.committeechairO'Brien, Walter F. Jr.en_US
dc.contributor.committeememberTafti, Danesh K.en_US
dc.contributor.committeememberSharma, Omen_US
dc.identifier.sourceurlhttp://scholar.lib.vt.edu/theses/available/etd-12222011-143750/en_US
dc.date.sdate2011-12-22en_US
dc.date.rdate2012-01-20
dc.date.adate2012-01-20en_US


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