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Exam 1 - J" 1 AE N3 DMWK EM#1 USE BLUE WK 1 Discuss...

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Unformatted text preview: J."- 1 AE N3 DMWK EM #1 USE BLUE WK 1. Discuss brie. 1: 111m; 1;: ea wp' ch dcambé. res: fiwtifln fipw untity. LSnppmafimmhflmmwhcmhgimgmcflmfimofflflflflwhfiq 6.11 Worm.p=l41pfia.andT= .Bflj’F. Calculalcthcmrhukncchmand mmmmhmHm Womalhishcmmmfur model Inning {ufifin}? LIE-5., I;?, W 3. Gimp=ilflflztiipfifirmtltemp=1m.fli3.fl°F.wflufl:thedmsitynfnirmd 1h: uncertainty in the: valuc DI the densiljr. .. Gag.” i”? 1; ‘nomp .163 fly/ I r’ 4. Apiwt tub-n: racism sundaflniru Ilflmflupcrhour. A water mannmntcris WmiLHu‘wmmfinthfiquflcrwiflbcindicuflfl 5_9§ 5P4} mans Testl Open Textbook Use Blue Book I. mmeflhafinflmhlmuH: Re: 1o?pum:nmpamorofi=. 255: fifth”: 2. Dflmiootbohonrpownrmqoimdtoopomoawiodlmdwilhlniflflhy 121] 11. lost aeolian under the following modifioos: loll. motion spud a 115 mph. firmmmmmdairpmsumintmmonm Iflfl‘FandHJpsia. rospecfivcly, motor-propcller officimcy = 9.35 overall energy min ER: = 5.0 2 I 70;: in p 3. Suppose the following data at: obtained in a wind mung! tos't of an airfoil: lb _ 20.1 i ‘2 furrow} qHBGAiflA M1 “1.0013111 Colonial: the Iifi oooffioiool C; and in error bounds. Ff Twins; :..¢=':f5' AE 3&3 Open Textbook TEST Hill Use Blue Book "f.Siqiposesnflhflfiflflizairfoflisteetedotakcynoflsnmberoffimmmafiod mmcmu=u Ushglhemeflloddevehpedbyfimnlaoohsfm mmmmlHtmdncieuIIReymflmofmm. '-75 1. Suppose that a supersonic wind tunnel has test section cross-seedonal area 36.00 in3 and throat area 20.45 inz. “do: stagnation {total} pressure 13ml} psi gage. The annosphnrie pressure is 14.6 psi. Find the test section Mach number, and the stalil: pressure in the test session. L {J £3 - -+ .r Iaenla'ople flow properties- 13-0!P5L1 .I-I ._.. a 4" -vl|.H H I”: 1f.- p .9 anon-rot MI“ «rfl'l m1 will Illflfla-fll. M555 I-Gl 11.3344“ BE" wilt «Gm-{DI M3]? i—fll tun-emf IBM-Hill EH! «I-fll o.aoar+ol 1} I73] 44'" ilLlflIH-fll QIMI-fil ilflflwlrfll [III-1511?“ fllfll-I-OL {LIME-LN '11?” H}! {1?555 r51 lid-IE 51 Hi] QIMJ-D! {11693 d-fl'l fi'JflW-l-fll 9.?IH+U: fififlfli-l-GII DJSIIG-l-flll U-JflT-rflI .nzosn so: filo-SIM“ nam- +ol o Isak-m: o nso- or onion — o: name or n aaso +o1 nisa2+sl on}: an: new t or on +01 on}! an o 9:4 as: ems out emu-oi 11mm: HEB-iii elitism: one...“ omen: dim-Hr: new-+13: ozone-or omits-m onion —o: nus: +9.1 fififl‘lfiH—Dl us: All 01193 +11" 0.23m +I.'.'rI M35} +112 QHJSHH Elm-i +o| 913295 Hill onion +01 did-i2 +131 onions: c.2152 +fil Manhol MESH-hm nlsol +412 Mlle-+1}: Mallow: Ellifl+fll snows: 0.1m m: on»: +o| DESI-rill mum Note: ”+01" meson "multiplyr by ID“, “HE“ means lolliply by mo. &; Awingmodelwithospertralioltaperratiofljflnndsyasnfljnehesistestedinn closedreoiaogolnrleatsunionofheightfi feetmdwidlhlf-Iqet. Atnngleofanaek EIWfltliflmefidmhMCL=lm ._.,, {a} Calculuetln: angle ofattoek corrected re: downwah. 3.15 {a} lrcpnrnmsomnemnmscnlso.mmewuemmcd for downwash- mf‘fl-P 4. Suppose the pitching moment is measured at the 10% chord location. yielding the following data: o CI. Cu B ° I}. 1 I H) {1.2236 3 ° 0343!} 0.1041 WEWMMmioeflimuamofehmdhefindm I..- l?- — - For- ABM! Dpchenhauk :1an TEEI'ND.2 1. Asymcuidfiuuhlcwndgcahfnilismummglequmiahmm fnmmpmufmcuppumfampmfldwmmcfim-m Stuck mMmmmmhsmrmM-fimmfimflflow. Alamskemh : mainline passing above 1h: airfail. and mac beluw. Indicate: whm Mumminmmm MMWfiW ‘2. Anahcmflwimmmmmaffifiisdmgmdmflyazmfllm- Amndclufthc airmflwimmmmufflflfihismhclesledmawmdnmnclmmwfltm @5315:me Wfllmmmlubcmminghl? Explain- M: : :jlfi- (IN) ML 2. 2.1mm W' I II; - _ _ 2 EvfluauthnflswfldEffiniuncyfanmnmgfij—Cumh+lfle(q (cl-mining) {m 1 wing of aspect min 3. for which the fun-wing data mm uhminnd: 3”; ‘35. Amumfinedbofiyufmmlmiunisminawhflmduq=fifllhffi1 Th: Marianffllcmudelisflflfl.thclcngflluflhcmudflisontfuflt.tha WfiMEmmfcmmmmflfidfl-mgmnfiuis 1-.'J'5 talcum: lhcvalnenfqmrmctedfurmlifiblochgn. 1*, '15 3,37% ...
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