Boundary Lyer Theory

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786 Bibliography A I). Progress hr Aeronautical Sciences, Pcrgamon Press, London (only contributions to fluid mechanics listed) Vol. I (lSIil), ed. by A. Forri. D. Kiichernnnn nnd L.H.G. Sterne Mmkell, E.C.: On t.lm principlw of acrodynnrnic design. p. 1-7. Legendrc, R.: Celcrtl den profils d'nuhcs pour turbomachines t.ranuuoniques. p. 8-25. Fennin, M.: l,n thkorie den 6couletnent~ b potent.icl I~omogPno ctses applications an cnlcul den ~ en rhgimc ~uperaonique. p. 20- 103. C R Becker, E.: IrtstationRre Grcnzschiclltcn hinter Verdicl~tungsat~sscn ontl Expansicna\vcllen. p. 104- 173. Goldworthy. 1P.A.: On 1110 tlynamicn of ioni7.cd gns. 1). 174 --205. ~nrron, C.l1.E., and Randall, D.C.: The theory of sonic bnngs. p. 238-274. Vol. I1 (1962), ed. by A. Forri, D. I
Clementa, lt.R., and Mad, D.J.: The rcprescntntion of sheet8 of velocity by discrete vorlices. p. 129-146. Chuc, S.Jg.: Prrsst~re probes for fluid n~rasnrcmentn. p. 147-223. Tanner, M.: Reduction of bnse drag. p. 360-384. Cnrricre, P., Siricix, M., and Delory, J.: MBthodes de calcul dcs Bcoulcment turhulents d6coll(?c~ ct suprsonique. p. 385-429. Vol. X VII (1976/77), ctl. hy I>. ICiichemann Broadbent, E.G.: I'lows with heat addidion. p. 03-107. Jones, I). S. : Thc mnthcmnticnl theory of noise ~hiolding. p. 149 -220. Broarlhcnt. 1C.G.: Noisc shickling for aircraft.. p. 231-268. Glms, J.J.: Shock waves on earth nnd in spncc. p. 260-286. Tanetla, S.: Visunl study of unsteady acpnratcd flows around bodies. p. 287-348. A 4. Advaneen in Aeronnntical Sciences I Vol. I ond Vol. II. T'roccrdings of the First Tntcrnationnl Congrcss in Acronn~~tical 9 CICtlCPR, ' Mndrid, 8 -13 Srptetnbcr, 1958. I'crgamon Press, London, 1959. Vol. III and Vol. I V Procredings of tho Second Tnkrnntional Congrens in t\cronautical Sciences, Zi~rich, 12 - 16 Septenrhcr, IWO. Pergan~on Press, I,ondon, 1962. Vol. V: Proceedings of tho ThirdCongrms of the lntornntional Council of the Aeronnnticnl I 'I rlcnces, ' Stockl~oln~, 27 -31 Augrwt, 1962. Spartan 13ooks. Wnuhington J).C., 1964. Vol. VI Proreedings of the Fourth Congress of the 1ntcrnat.ional Councrl of the Acron~utiral Sciencw, l'nris, 24-28 August, 1964. Sparlnn Books, Wnshington D.C., 1065. Two Volnnie~ Aer~spn~ePr~rccdings 1966: Proceedings of the Fifth Congrcas of the International Coimcil of tho Acronnutirnl Scicnccs, London, 12-10 ScpIamhc.r, 1066, cd. by Tho Royal Arronnut.irnl So(-irLy nnd McMillnn, Imldon, 1067. R. Ilnedhooks, Collected Pnpern, Applied Mechnnies Congresses Princeton University Serie~ on High Spccd Acrodynnmics and Jet Propulsion, ~rinceton University Press, I955 -1964, Vol. 1 to XI1 Vol. 1 (1965), cd. by 1P.D. Rosnini: Thermodynamics and physics of matter. Vol. 11 (1.9*56), rtl. by 11. Lcwi~. R.N. Pcnac, 11,s. Tnylor: Con~hustion processes. Vol. 111 (1958). cd. by H.W. R~nn~nns: Funrlan~entals of gns dynan~ica. Vol. I V (l964), ctl. by F.K. Moore: <strong>Theory</strong> of lnrnil~nr flows. (=onlril~ulions h?/: Moore, l7.lC.: 1ntrotluct.ion. 1,ngerslrorn. P. A. : 1mni11nr llow l.hcory. Mngcr, A.: TI~reo-ditt~ct~nional Intninnr boundary Iaycrs. Rott,, N.: <strong>Theory</strong> of tin~c-dcpcntlcnt laminar Bows. Moorn, F.IC.: Flypersonic boundary laycr theory. Ostrnrh. S.: 1,ntninar flow with body forces. Shen, S.F.: Skl)ilit.y of Inminnr flows. Vol. V (19.59), ed. by C.C. Lin: Turbnlcnt flows and heat transfer. Contrbvtionn 6!y: Drytlen, 11.L.: 1'rnnsit.ion frotn laminar to t,urbnlrrlt flow. Srhnl)nunr, G.R.: Turbulent flow. Bibliography 789 Lin, C.C.: Statistical theories of turbnlence. Yachter, M., and Mayer, E.: Conduction 01- heat. Deissler, R.G., and Sabersky, R.H.: Convective heat trnnsfcr and friction in flow of liquids. VR~ Driest, E.R.: Convective heat transfer in gases. Yuan, S.W.: Cooling by protective fluid films. Penner, S.S.: Physical bunis of thermal radintion. Hottcl, H.C.: Engineering calculations of rndiant hcnt exchange. Vol. VI (1954), ed. by W.R. Sears: General theory of high spced aerodynamics. Vol. VlI (I%57), a d by A.F. Donovan and 1I.R. Lnwrcncc: Acroclynnmic componontn of air.. craft at high speech. Vol. Vlll(1961), ed. by A.F. Donovan, H.R. Lawrence, F.E. Goddnrd, and R.R. Gilruth: High speed problems of aircraft and experimentnl methods. Vol. IX (1!?54), ed. by R.W. Ladenburg, B. Lewis, R.N. Pease, and H.S. Tnylor: Physical rncnsnrementm in gas dynamics and combustion. Vol. X (1964), ed. by W.R. Hawthorne: Aerodynamics of turbincs and compressors. Vol. XI (1960), cd. by W. R. Hawthorne and W.T. Olson: Ilcsign and perforrnancc of gas turbine power plnnta. Vol. XII (ISc59), cd. by O.B. Lancaster: Jet propulsion engines. Ilnndbucl~ der Phynik, ctl. hy S. IPliiggc, Springer Vorlng, Ik:rli~~/(l;iit,t~i~~l/IIt~itIeII~org Vol. VIIIII (I%!?), Stromungsmechnnik I Oswntitmh, I
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McGRAW-I4ILL SERIES IN MECHANICAL E
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vi Contents CIIAPTEII V. Exnct ~olu
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Y Contents A " I XI X 'I'lirorrt.ir
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xvi I'orcworcI Thc result was t.11~
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From Author's Preface to the First
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the aid of thorctical considcmtioti
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even in fluitls wit,lt vcry srnall
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10 I. Or~llinr of lluicl rnot,ion w
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The vclwil y IL at some point i11 t
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Fig. 1.6. Firld of flow of oil nho~
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22 I. Outliric of fluid motion with
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2 (i TI. O~~tlittr of Imun~lnry-lsy
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Fie. 2.511 Fig. 2 .5~ Fig. 2.5b Fig
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S - point orscpnrnt.ion T'ig. 2.12.
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3 8 \ Y?\ If. 011tli11e of boundary
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42 11. 011tli11e of Iw~~ntlnry-Inyr
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[:j2a] I?o~cilhrntl, I,.: Thr forn~
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50 111. l)crivnt,ion of thc cquntio
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Fig. 3.3. Tmcd clintor1,ion of flui
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of flltitl is strcsscd in thrcc nlu
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1:i~ 3.8. Qltnsintzt.ia cotnprrssio
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66 111. 1)wivntion of the eqnntions
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CHAPTER I V General properties of t
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74 TV. Gencrol proprtic~ of tho Nov
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Ilcre v, c, :tntl k tlrnol,c 1.I1t:
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conclil.ion (4.14) plays n part wl~
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86 V. 1':xact solul ions of tlir N:
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90 V. ICxnct sol~ttion~ of tho Nnvi
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94 V. Exnct sohltiono ol' tho Nnvic
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Table 5.1. Functions occrtrring in
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11. Flow taenr n rotnting disk. A f
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106 V. JCxact solutions of the Navi
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cnu bo npplirtl nt mont, nn fnr RS
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114 VI. Vcry slow motion where r2 =
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1 I8 VT. Very slow motion r. 'l'l~o
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122 VI. Very rrlow motion ext.endcd
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126 VT. \'cry slow rnot.ion Part B.
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130 VII. Boundnry-layor cquntionzl
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'1. Skin friction \VlIat1 t.11~ I)o
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138 VII. no~~ndnry-layer cqnntions
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142 VII. Hor~nclnry-lnyrr rq~~ntii~
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146 VII. I~o~~ntlnr~ Inyrr cq~~ntio
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CIIAFTER VIII Gencral propertiee of
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164 VIII. Ccnernl propertic8 of Lhe
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158 VIII. General ppropcrtics of th
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VIII. General propertien of the bou
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'I'his c.quat,ion Lmnsforms into t1
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170 TX. 1Sxact uolutions of t.ho st
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174 TX. Exnct ~olut,ionu of tho sto
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178 IX, Exact solutions of tlrc ste
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and t,llc? clnsh now clet~otos tlil
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1 86 10 0.8 0.6 0.4 0.2 0 -0.2 -0.4
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ccnt,rred nt, (m -1- 1, n). 1'110 t
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194 IX. Jqxnct eolutions of thc stc
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O~l:cr ehnpw: Second-order cITcetls
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202 X. Approximate rncl.hoda for st
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206 X. Approxitnnte rnct.l~otls for
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210 X. Approximate mcthod~ for shad
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214 X. Approximato mothotls for sha
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218 X. Approximntn met,hods for shn
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222 X. Approximate methods for stea
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220 XI. Axinlly symniobricnl nnd th
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230 XI. Axinlly symmctricnl and thr
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23.1- XI. Axially uynimet.rira1 nnc
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the two wries expnnsicws for sin (%
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242 XI. Axially nymmct.riral and tl
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in cross-flow, tlrprntls only on lh
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250 XI. Axinlly nyrnmet,rirnl nntl
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XI. Axinlly ~,vn~n~et.rir;~l nnrl I
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258 XI. AxhIly syn~rnrtrirnl nncl t
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. . lit 1 h1:lgt.r. '1.: 'l'l~idc I
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206 XIT. l'l~rr~nnl bo1111r11iry ln
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270 XIT. 'I'l~rrtnal boundary layer
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can I)r rct.ni~rrvl in inrotnl~rrss
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if wc: pillf - - 'I1, - (A7'),. 11,
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Rotntirig rli~k: (:II:I~I. V, in pn
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286 X11. 'IY~rrrr~al bo~~ndnry laye
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290 XlI. Tl~rrnmal boundary layers
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with 0,' -. () at, r] - 0 and 0, =
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2!)H XI[. Thcrn~al bor~nrlnry Inyrr
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302 XJI. Therninl boundary layers i
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306 XII. Tllcrrnal hor~ndary layers
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310 XJI. 'I'hcrmnl boundnry layers
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314 X11. Thermal boundary laycrs in
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318 XIT. Tl~crnial bonndnry layers
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322 XII. Tl~or~nnl I)onndnry lnyers
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326 X l I. 'l'l~crn~nl hounrlnry ln
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330 X[[1. lmninar bor~ndnry lnyers
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334 XIIT. Lnrninnr 1)oundary laycra
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338 XI I I. Im~linnr I>orirtclt~ry
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342 XI11. Tmninnr Imlndary layeru i
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346 XI 11. T,ntninar I~or~nrjary hy
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350 XIII. 1,mninnr honnclxry lnycrn
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354 XI 11. 1,nminnr h~nrlnry 1:ryrm
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Fig.. l3.16. In 13.18. lain~innr ho
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a Intninn.r l)out~rlary I:~.ycr, bu
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1 I Itc vnriolts c4Twl.s ol'sl~oclt
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370 XIIJ. I~tminar boundary layers
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\'all I)rirst., 15.11..: 'l'hr prol
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CIIAPTER XIV Boundary-layer control
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5. J'rrvrntion of trauaitinn by the
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frorii th; 1c;ulitig rxlge! (l3l:wi
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390 XIV. Ilo~~n~lnry-lnycr contml F
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. - v, (x) =cons/ Fig. 14.14. 1,ant
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invc?st.igai.ctl. In this msc too,
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402 XIV. Dounclery-layer control 1.
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Ni\('A 'rM !I74 (1!)41). 1861 Sinli
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110 XV. Non-~teldy bortndnry layers
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414 XV. Non-st.cncly hour~tlnry Iny
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418 XV. Non-slmrly l~orrnclnry Inyr
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422 XV. Non-st,cndy hoixnd~ry Inycr
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420 XV. Non-nl,mdy Fig. 15.58 Fig.
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XV. Non-utcncly boouclary lnyers wh
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434 XV. Non-stcxcly boundary layers
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438 XV. Non-atcndy boundnry inyer~
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442 XV. Norl-st,aady boundary Isycr
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440 XV. Non-st,rndy ho~~nclnry laye
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450 XVI. Origin of tnrhulence I pyi
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XVT. Origin of turbulcncc I n. Some
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458 XVI. Origin of turbulence I b.
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462 XVI. Origin of tnrb~rlmcc 1 num
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466 XVi. Origin of t.r~rhr~lrncc 1
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470 XVI. Origin of h~rlwlcnce T I R
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474 XVI. Origin of l,t~rl~~tlct~rr
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478 XVI. Origin of I.rtrb~tlmcr 1 t
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482 XVT. Origin of tmbulcncc I c. E
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486 XVI. Origin of k~rbulenre I 148
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490 XVII. Origin ol t,urbulencc 11
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404 XVII. Oriein of tnrbnlencc TI F
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498 XVII. Origin of turbnlmco II t,
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Tlw tlisl.nr~cc Iwt,wccn the point,
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c. Efict of ~urtintl on trnt~nition
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510 XVl I. Origin of Idmlrnro I I '
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514 , XVII. Origin of turbulence 11
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518 XVI I. Origin of turhr~lcncc 11
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on the bnsis of t.hc tl~corct,ical
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626 XVII. Origin oI t.11r011lonco I
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630 XVII. Origin ot t.~~rhr~lrncc J
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XVII. Origin of t.urh~~lencc TI 7 !
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638 XVII. Origin of t~~~rbnlc~~rr I
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\vi(,l~ a (-ylit~(lw envcrv(1 wiI.1
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646 XVII. Origin of turbulence TI F
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550 X\'ll. Origin of t,11rh111rnrc
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554 XVII. Origin of t,rlrbuloncc TI
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558 XVITI. Fundamentals of tr~rbule
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562 XVlI1. R~nclnmont.nIu of tur1)u
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The corrrlnt,ion co~ffiricnt~ y~ ra
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670 XV111. I'nntlntnrt~t~nlrr of tt
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574 XVIII. 1'undnnient.alu of tnrl~
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CHAPTER XIX Theoretical assumptions
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682 XIX. Thcoroticnl wsltmptionu fo
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586 XIX. Throretical aaotin~ptiona
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5l)O XIX. Tl~rorrt,icnl nmumptions
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594 XIX. 'rheoreticnl nssornptions
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698 XX. 'I'~~rl~ulrnt flow f,lrro~~
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602 XX. T~rrbulcnt flow thro~tgh pi
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606 XX. 'l't~rhl~lc~rit flow thro~~
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GI0 XX. Turbulent flow throngh pip
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Icror~~ ()I(, phj.sic*:~l ~)oint. o
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620 XX. Tnrbnlcnt flow tlvough pipe
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dimensions Fig. 20.26. 1tc.sist.anc
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628 XX. T~lrbnlmt flow through pipe
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632 XX. Turhulcnt flow through pipc
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636 XXI. Td~nlcnt houndnry layers a
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610 XXI. Ttrrbulent bor~ndnry layer
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644 XXI. Turbulent boundary laycrs
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048 XXI. Turbulent boundary layers
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652 XXI. Turt)~~lcnt houndnry layer
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656 XXI. Turbulent boundnry layers
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660 XX I. Tl~rhlent bo~~ndary layer
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664 XXI. Turbulent boundary layers
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CHAPTER XXII The incompreesible tur
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672 XXll. 'l'llc incon~prcssiblc tu
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070 XXII. Tlic incompreaaibto lnrl)
Page 351 and 352:
FRO XXII. Tho incornprcs~iblo turbu
Page 353 and 354: 684 XXII. 'Yhc incon~prcssible Lnrb
Page 355 and 356: 688 XXJI. The incon~prcssible t,urb
Page 357 and 358: 002 XXI1. Tho inro~nprc~sil~lo tt~r
Page 359 and 360: is prol)nt~t,iot~nl to the rnclius.
Page 361 and 362: lf$8] Mucsm:tnn, 11.: Z~~snrntncnhn
Page 363 and 364: 70-t XX I1 I. 'Ihrbulcnt bonrwlnry
Page 365 and 366: 708 XXIII. Turbulent bonndnry Iaycr
Page 367 and 368: 712 XXI 11. 'I'~~rl~~~lemt bo~~ntln
Page 369 and 370: 716 XXIII. 'I'urbr~lcnt bor~ntlnry
Page 371 and 372: 720 XXIII. Turbulent boundary layer
Page 373 and 374: 724 XXlll. 'rur1)ulcnt boundnry Iny
Page 375 and 376: [04] Smith, P.D.: An integral predi
Page 377 and 378: 732 XXIV. Frcc trtrbt~lent flows; j
Page 379 and 380: 700 XXIV. Prrc tr~rb~tlent flowa; j
Page 381 and 382: Neglecting u12, we obtain XXIV. Prc
Page 383 and 384: 744 XXIV. lhc L~trl)ulcnt Ilow~; jo
Page 385 and 386: 748 XXIV. Free turbulent flowa; jet
Page 387 and 388: 762 XXIV. Frcc td)ulcnt flows; jcta
Page 389 and 390: 756 XXIV. Prrc torbulent flows; jet
Page 391 and 392: 760 XXV. DotcrminnLion of profilo d
Page 393 and 394: 764 XXV. I)ot.crtninntiotl of profi
Page 395 and 396: 768 XXV. Determination of profile d
Page 397 and 398: XXV. 1)obrlninalion of proRlo drag
Page 399 and 400: 776 XXV. 1)ctormination of profile
Page 401 and 402: A. Reviews organized in serial publ
Page 403: 784 Bibliography Sherman, I?. S., I
Page 407 and 408: 792 Bihliography 13ird, R.R., Slewn
Page 409 and 410: Oswatitach, I
Page 411 and 412: H:I:IR, 11. 776, 777 Ilnnsr. 1). 62
Page 413 and 414: Scl~crb:trl,l~, I
Page 415 and 416: 805 811bjrct lntlrx 209, 354, 385,
Page 417 and 418: 812 Snhjcct lntlcx - vorl.irrs 526,
Page 419: List of most commonly used synibola
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Boundary Lyer Theory

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