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Investigation of the shock wave/boundary layer interaction of scramjet intake flows (Berichte aus der Luft- und Raumfahrttechnik)

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en Limba Engleză Carte Paperback – July 2010
Thisthesisaimstoextendtheknowledgeofscramjetintakeflows,especiallyoftheSWBLIphenomenonundervariousfreestreamconditionsandotherinfluences.TheSWBLIisconsideredparticularlyasitoccursinawiderangeofflowsspanningfromthetransonicoverthesupersonictothehypersonicflowregime.Theseflowsoccure.g.atthesupercriticalwingemployedinmodernaircrafts,thecontrolsurfacesofaircraftsandmissilesflyingatsupersonicspeedsaswellasthere-entryvehiclesliketheSpaceShuttle.TheresearchonSWBLIsstartedmorethansixtyyearsagoandisstillanimportanttopicoftheongoingresearch.Atpresente.g.theheatloadandthedragofatwo-dimensionalscramjetintakewithasharpleadingedgecouldbeestimatedevenwithoccurrenceofaSWBLIprovidedthatthesizeoftheSWBLIisknown.However,sofarnoanalyticalpredictionmethodexistsforthesizeofaSWBLIwhichdependsonvariousflowsimilarityparameters(e.g.theMachnumber),butafewcorrelationswithaspecificscopehavebeendeveloped.Theseparameterschangesignificantlyforaspacetransportationsystemacceleratingandpassingaltitudeswithdifferentatmosphericconditions.Duetothefactthattheflowsimilarityparametersalsoaffecttheflowphenomenaoccurringe.g.attheoutercompressionrampswhichalsoinfluencetheSWBLIsize,athoroughunderstandingofthesephenomenaandtheflowsimilarityparametersoftheSWBLIarerequiredforthescramjetintakedesign.
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Specificații

ISBN-13: 9783832291877
ISBN-10: 3832291873
Pagini: 200
Ilustrații: 19 farbige Abbildungen
Dimensiuni: 149 x 211 x 12 mm
Greutate: 0.27 kg
Editura: Shaker Verlag
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