Annasaheb Dange College of Engineering and Technology, AshtaTal - Walwa, Dist-Sangli; India 41 !"1Department of Aeronautical EngineeringCOURSE DETAILSStructure of CourseClass TE-#art-I Se$%-&Co'rse Code and Co'rse TitleAE()S#ACE #()#*+SI),-IDesignated as Co$-'lsory#rere.'isite/s 0S1"!,0S1"1Teaching Sche$e 2+ect're/#ractical/T'torial/Drawing3 "!/"4/""/""Total Contact 5o'rs6 Theory/#ractical/T'torial/Drawing 44/14/""/"" 5o'rsCredits "4E7al'ation Sche$e6 Theory #a-er/TW/#)E/#) 1""/48/""/""Course Educational ObjectivesCEOs!"The co'rse ai$s to6C-I To introduce aircraft -ro-'lsion thro'gh initial history and 7ario's -ro-'lsions syste$s%C-II To introduce theory differentiating aircraft -ro-'lsion syste$s thro'gh 7ario's $eans%C-III To impart awareness on ther$odyna$ics of 9et engines and 7ario's i$-ortant co$-onentsCourse Outcomes COs!" *-on s'ccessf'l co$-letion of this co'rse, the st'dent will be able to61Distinctly 'nderstand the classification of -ower -lants and differences of 7ario's -ro-'lsion syste$s incl'ding 9et engine and roc:et engine%4 5a7e a f'nda$ental :nowledge t'rbo9et, t'rbo -ro- and t'rbo fan engines%!*nderstand conce-t of ther$odyna$ic analysis on co$-onents of 9et engine% (a$ 9et and -'lse 9et a--licationCourse S#llabusSECTIO$%IUnit &" 'LI()T *RO*ULSIO$% AIRCRA'T (AS TUR+I$E E$(I$ES% (E$ERATIO$ O' Annasaheb Dange College of Engineering and Technology, AshtaTal - Walwa, Dist-Sangli; India 41 !"1Department of Aeronautical EngineeringT)RUST% E$(I$E *ER'OR,A$CE *ARA,ETERS5istory offlight -ro-'lsion,(oleof reci-rocatingengines%)-erating en7elo-e offlight 7ehicles% Engineo-erational li$its% Air breathingengines- ty-es, Aircraft ;as t'rbine engines- ty-es, o-erating-rinci-les, disting'ishingfeat'res, sche$aticdiagra$s, relati7e$erits, anda--lications% Engineco$-onents- f'nction, sche$aticdiagra$, layo't, and Engine station n'$bering, Thr'st generation- $o$ent'$e.'ations, ;ross net,'ninstalled, and installed thr'st, and -ro-'lsi7e efficiency% Engine -erfor$ance -ara$eters- s-ecific thr'st,s-ecific f'el cons'$-tion, total efficiency- -erfor$ance trends% Effect of flight conditions, 9et e ?a9or feat'res of e I$-ortant factors affecting co$b'stion cha$ber design >Co$b'stion -rocess > Co$b'stion cha$ber -erfor$ance%*ER'OR,A$CE SE$SITI4IT5Effect ofo-erating7ariableson-erfor$ance-=la$et'becooling-=la$estabili@ation>*seoffla$eholders > ,'$erical -roble$s%-. )rs!Unit 6" $O77LESTheory of flow in isentro-ic no@@les - Con7ergent no@@les and no@@le cho:ing > ,o@@le throat conditions >,o@@le efficiency > +osses in no@@les > )7er-e Thr'st re7ersal%-0 )rs!Unit 0" CE$TRI'U(AL and A8IAL 'LO9 CO,*RESSORSCE$TRI'U(AL 'LO9 CO,*RESSORSCE$TRI'U(AL 'LO9 CO,*RESSORS#rinci-le of o-eration of centrif'gal co$-ressors - Wor: done and -ress're rise -&elocity diagra$s -Diff'ser 7ane design considerations > Conce-t of #rewhirl >(otating stall%A8IAL 'LO9 CO,*RESSORSEle$entarytheoryof a&elocitytriangles >Degree of reaction- Threedi$ensional flow > Air angle distrib'tion for free 7orte< and constant reaction designs - Co$-ressorblade design - Centrif'gal and A Effect of -ress're, 7elocity and te$-erat're changes of air entering co$-ressors%+T C0, AS, CT&& ?ethod of thr'st a'g$entation +T C0 AS, CT&/Characteristics of t'rbo-ro-, t'rbo9et > #erfor$ance characteristics%+T C0, AS, CT&1 ,'$erical +T C0&2 ,'$erical +T C0, AS, CTIII&6Internal flow and Stall in S'bsonic inlets - 0o'ndary layer se-aration > ?a9or feat'res of e Co$b'stion cha$ber -erfor$ance%*ER'OR,A$CE SE$SITI4IT5+T C0, AS, CTUnit Lect? $o?Lesson *lanT, TA AT,apping >it ,o@@le throat conditions+T C0, AS, CT4 a,e/@,o@@le efficiency > +osses in no@@les > )7er-e Thr'st re7ersal% +T C0, AS, CT4I /A #rinci-le of o-eration of centrif'gal co$-ressors +T C0, AS, CT8 a,e1- Wor: done and -ress're, &elocity diagra$s% +T C0, AS, CT1&Diff'ser 7ane design considerations > Conce-t of #rewhirl >(otating stall%1/Ele$entary theory of a &elocity triangles > Degree of reaction+T C0, AS, CT4 a,e11Three di$ensional flow > Air angle distrib'tion for free 7orte< andconstant reaction designs - Co$-ressor blade designC012 Centrif'gal and A