UNCLASSIFIED

AD NUMBERAD378494

CLASSIFICATION CHANGES

TO: unclassified

FROM: confidential

LIMITATION CHANGES

TO:Approved for public release, distributionunlimited

FROM:

Distribution: Further dissemination onlyas directed by Director of SupersonicTransport Development, Federal AviationAgency, Washington, DC 20553 SEP 1966 orhigher DoD authority.

AUTHORITYFederal Aviation Agency ltr dtd 23 Feb1972; Federal Aviation Agency ltr dtd 23Feb 1972

THIS PAGE IS UNCLASSIFIED

[I jal-

C'

)CLASSIFICATION CHANGEDTO UNCLASSIFIED

1 < .FROM CONFIDENTIALPER AUTHORITY LISTED IN

I FAA 1tr,TAB NC..72 ... 23 Feb 72[ DATE 15 Apr;l 1972

, . . . 9

BestAvailable

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sec, -cets~t which apply to thite 1*oCtaeut sud mac be &tt

prior ap7roval aRC r

Director of cupersc-nic fransport Daeloseent'I Pea Aviation hint,

Wastington, D. c. 20S53

The dtetribucia-a of this report ts hlite bease it corztains4 tccholczridentifiable with itnes e=Iigied from export by the U

irrecof Stare (U. S. Eapafl Control Mt of 1"S4, as aumAed),

AAWL

BOEING MODEL 2707.

PROPULSIO PERFOHON AANCC

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Federsl 20 JUtte 1%6 Phase III APstiLet for ProposaLAviation Agency

U, S. 1*2 Ui. S. Stwndar4 Atitspher.Gaverr'ant rinting Offic*

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of !Alet izztalled &ra& coefficients for CHLt aed accreentinm ist shown ini Fig. 23.

~ 311...32 Cim and4 Acc-lcnztios 5,tX&1rd Sy l~e . A ccapoittVcurve of inlet iiiaurnj ?rZvU hivns a1 a- own a1 1 fag for

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le'~~jcuefticlrnt. 'the inlet *iarc dreogis Se2i:iirX1IS. mm piliajs 4m

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* M.I.T, Technical Report 1' .T,%e sifazreyci betwcen th: theoreticral-ccmical floic ass flow ratio ahe the inlt oa-eratipa nos fl" ratiof(mor=a shock apillsg.) is shon-a in Fig, 2J. The 4dditive dral ~o-efficient for 142ch ruvhera abos.e 1.3 is sbc-.r xn Fig. 30,SJA.li2.4.2 fo Loc Co'Kcet thI lip sorties force

above i.f w:-t rzaicuilattd by the metls heen tAog -A D17842. TheP ratioof lip zuctiun force to a dditive ing is she 4 i, Fig. n2.

fr ~~ ~ ~ nc '- a. ... 2. aksi4e 0,& oeiiet The CawlitlRicsng th* vo2rtvx valva. 'Me ceeul boods y v bleed dras sLAlL be*

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fordr~g e titcs Th vnr~jlevel at the lelkage, aIr shAll be Thesaqne as fee te bvinary lajer bleed f tve u. 1ct coal pleans, Thecvntertaiiy boundar-y laykur bleed dr-ag shali Y Cbez p n21rercne~at kthe engine dlezan3 as% flow at t*Personic cnase.t This; shall ir-elude0.3 peOrcvnt leakagec for drag esrizates. The energy lvti of the center-

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14.1ksa T- -cfiitt Air-ci4itieeiog bltvd fera 15 theiaf

';,I...5 1 zrrssier ?j' er fut;d Total ,-.a-atlo. he" 40"*tr y y

btfed4 t ilts nsn ezvey o ari cv,= .;r dting at~m of .4 )tas± b*z

t arc skcaal in Fit. 51. Tlis era-ve ;s a rczt~spole hvn h tvt4lbleed mass fj;w rutio, and tL;; srbia fec bleti cenpoaasst toth4 total blee'd "*Se r"- raio t led .a'as flaw~ ratice ls s in

3S; W cc based,! I nlet UP~ fennl art%.

3.I,.1.2.1 r.I~iirt Laver Bleed Exit Th,-rt-st Coefficet-t. 7Uebcunday layer ble7& Znit thtst czieftiiitz fr AllX iet ?lecirrs rShwn in fig. Ud. All bleedj exit* shall becOOVe~get netLeOS dischars-

ing at I b~eg ftan the Inlet uAis.

t&'irh 0 Fx. ,~a a dag ostx~ig i th su o~f bypas nats

-* drag cz-fflciens ard louverr oflxtrl w~ave drag.

chssin Fig. Is. At ii, the stream tute area otf the tbypass floe based

ixn brt ir density and vtlocityr upltrtamf oC the inlet.

3.141.26.2 Lcnier Wv DrefZ CoriLficlart. The estinated enameallossear WIF*v c--Uza- sesa -Siw n m tg. AS.1= louvewr eases-nal pressure Isbased cm o~as~in!oliu hc rssbrz lanzhips jlhaf. N.A.C.A.Repor NSc. .±n) with flcilte- as-rct yaxti prrs!asae relsef (Itf. Mccnta-

111 n ceri, $sproi Andn~lc)~~e n obique Sho-Le tax b~e-a sumtgii-od 6)a"v of .na fir,- lo fs . Fr conditions weno a P.crnC2 shoc'

Stands glse- Cf the itr, o uv~ner.tsiet average hlawer ce-tea-na preasa.rs

and 1054.

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