1954MNRAS.114..210S THE BENDINGOFASQUAREPLATEONSPHERICALFORMER at thesuggestionofDrE.H.Linfoot,deformationaphotographicplate certain assumptionsweremade,andsimilararemadewhereappli- this papersquareplatesareconsidered.Whendealingwiththecircularplate in aSchmidtcamera.Inthatpaperonlycircularplateswereconsidered. tioned inthesectiononboundaryconditions.Thesolutionforsquareplate cable inthispaper.Themodificationsappropriateforasquareplatearemen- transverse pressure. is, ofcourse,morecomplicatedandmuchthesimplificationduetosymmetry is lost.Theproblemis,however,showntobeequivalentinthemathematical sense totheproblemofbendingaclampedsquareplatebyuniform bent bymeansofaframesothatitisincontact atallpointsofitsedges,witha matically inFig.1.Rectangular axesNx,Ny,Nsaretakensuchthat Nx,Ny spherical former.Thestrainedandunstrained positionsareshowndiagram- © Royal Astronomical Society • Provided by theNASA Astrophysics Data System WITH APPLICATIONSTOTHEPHOTOGRAPHICPLATEOF Introduction.—In apreviouspaper*oneofthepresentwritersinvestigated, Displacements andstrains.—Theplatewhichis flatintheunstrainedstateis the presentwritersobtainednecessarycorrectionsappropriatetoa circular plate.Inthispaperthecorrectionsforasquareplateareobtained. for inmakingmeasurementsafterexposure.Inapreviouspaperoneof Schmidt camera,strainsareproducedintheplatewhichmustbeallowed Fig. I.—Diagrammaticrepresentationofthestrainedand unstrained statesoftheplate. When aflatphotographicplateisbentonsphericalformer,asinthe IV. M.ShepherdandD.Radenkovib * W.M.Shepherd,M.N.,113, 450,1953. (Communicated byE.H.Linfoot) A SCHMIDTCAMERA (Received 1954February22) Summary 1954MNRAS.114..210S x No. 2,1954Thebendingofasquareplateonsphericalformer211 of contactNtheunstrainedplateandformer.Thedisplacements the displacementwofapointS(#,3/,o)isgivenbyordinatez equations* (i). so thatthedisplacementsaresmallandwillberelatedtostrainsby point (x,y,z)inthemiddlesurfaceofplatearew,v,wparalleltoaxes Nx Ny>Nzandthecorrespondingstrainsinplaneofplateares,o^. (x,yyz) ontheformer. are intheplaneofunstrainedplateandNzisinwardnormalatpoint 0 where Ristheradiusofcurvatureformer. the platevanishes.Forreasonsgivenin previouspaperzzcanherebe be likewisenegligible.Herewemaywrite coefficient offrictionisremarkablylarge,the surfaceshearstressesxz,yzwill are foundtosatisfythecompatibilitycondition yx assumptions thatyzvanishonthefacesof theplate,andmeanzzacross neglected incomparisonwiththestresses planeoftheplate,andunless Airy stressfunctionx(>y)fromthebody-stress equations,followingtheusual the meanstresses'xkyyy,ïyinplaneof platecanbederivedintermsofan may bewrittenintermsoftheoriginalposition oftheelement.Itfollowsthat small theequationsofequilibriumanelement oftheplateinitsownplane © Royal Astronomical Society • Provided by theNASA Astrophysics Data System 2, The platesubtendsonlyasmallangleatthecentreofcurvatureformer If smallquantitiesoforderhigherthan{xfR)areneglectedinthestrains, Equations (i)nowtaketheform To therequireddegreeofaccuracywisgivenby On eliminatingthetwodisplacementsuandvfromequations(3)strains The differentialequationforthestressfunction.—Since thedisplacementsare * Cf.S.Timoshenko,Plates and Shellspp.304-5,1940. y xv =—5, — 2 oy~ 2 d*» ,_^ =(A dy dxdxdyR^ Sx+ Sy '~ dx2\dx)’ dy+2\dy) or Sy=+ Sx=+ ty 2 dx 2 xy 2 2 + 2 w =(x+y)¡2R du i/dw\ dy d+dx* du dvdzv dv i/dw\ y x +2 yy=^' dy^~ dxR' du dvxy du i dv I 2 d X R, R, y\2 X vy= — dxdy ° X -TO (5) (I) (3) (2) 1954MNRAS.114..210S 212 The straincomponentsin(3)areindependentofzsothatthemeans stress-strain relationsforthestressesinplaneofplateare stress function where £*, (7> (8> (9) 1954MNRAS.114..210S it followsthatequations(11)maybewritten No. 2,1954Thebendingofasquareplateonsphericalformer213 the coordinatesxandybyrelations=rcos,—rsin.Instrained or coordinates (/*,)intheplaneofunstrainedplateapointSarerelatedto 0 state thepointSmovestoanddisplacements inthedirectionsrand the Cartesiandisplacementsbyequations increasing arerespectivelyuandasshown inFig.2.Thesearerelatedto The correctiontotheposition angleisthengivenby 0 r © Royal Astronomical Society • Provided by theNASA Astrophysics Data System Radial andcross-radialdisplacements.Correctionofangles.—Thepolar Since u=owhen#forallvaluesofyandv V= E) 0 v= ÍSydy- «=ic u =cos^sin<£(ux +vy)[r, uj =vcoscf)—sin(f>(vx —uy)/r. r () y I c ydd ?Ä-.lÄ 2 dv 2y2 2 6R’ dx Edy6R' dy Edx S^ =u/r. (14) 4 Fig. 2. 2 x“ 6R’ (12) 1954MNRAS.114..210S 3 where the line=Jtt,sothatv{x,y)—u(y,x),weneed onlyevaluatethedisplacementu equations (12)itisfound,aftersomemanipulation, that for aquadrantoftheplate. where thenumericalvaluesoffirstfourcoefficientsEare taken intheform 214 W.M.ShepherdandD.RadenkovicVol.114 where displacement uofthepreviouspaper)is The actualelongationofthelengthNSmid-surfaceplate(the Without radialstretchingofthematerialplatecorrectionwouldbe m The totalcorrectiontotheoff-axisangleÀis JA, sothatthecorrectionduetostretchingonlyis 0 XC0S a 25 u =K2 *~ RW=i,B,5,...m*cosh(m7r/2) © Royal Astronomical Society • Provided by theNASA Astrophysics Data System ^ -K»»=1,3,5,... Xi“ m On introducingthestressfunctionxgivenby equation(17)intothefirstof (¿>) Thedisplacements.—Asthedisplacements are symmetricalwithrespectto {a) Thestressfunction.—Forasquareplateofsidethefunctioncanbe The stressfunctionandthedisplacements í 4 _ 2Ea _ 4¿?a -K (m1)/2 2Ea* ™(—i)~miryE m x <—tanhcoshsmh>, m—1,3,5, {- [2 2a) [mir ,mnmirxmrrx.mirx] ^ =0-3722;£3=-o-osSo;£-0*178;£7=-0*0085. — tanhcoshsmh mir ,mjTmiry. 5 t » 2 aj m7r 1,3,5,... ^ (W77/2)tanh(7^77/2)+2y{miry¡a) 2 co 1, 3,5,... 2 00 Asin m 12 K=^/ÄV, = (-1)^)/, A COS m 12 12 cos -Zcos ( -ly™)/mttx ( —^nvnx 2 cosh(rmrl'Z)a{nrnjof mirX m mr a a mny fsinh(mTTxja) x cosh(77777^/0)1 3 ZSOS=8A=| +|.(15) 0 £ i\z.(} = R€=R+Url6 4 +m 1 Trm cosh(7^77/2)a(77777/2)/ X =Xl+X2+X3>i?) m a cosh(miryja)ysinh(fmry/ö)l cosh(77777/2)a (77777/2)J 3 a cosh(tutt/z) A u r mTry') sinh —y m7iy\ 2> 6£ X* 1954MNRAS.114..210S 3 0 and No. 2,1954Thebendingofasquareplateonsphericalformer215 off-axis angleÀ(i.e.thequantitytobeaddedcalculatedfrom exposure) isgivenbySA=iTy,where2Rya,andmeasuredinradians. measurements oftheplateafterreleaseinordertoobtainangleÀattime errors duetoterminatingthesesummationsafterthefirstfourtermswillbevery small. The coefficientKisgiveninTableIforthefourteenpointsshownFig.3. By argumentssimilartothoseusedbyTimoshenkoitmaybeconcludedthatthe 1 by e=Ky*whereK%is givenbyTableII. given byTableIII.K iszerowhen<£=o°or45. ± 2y z © Royal Astronomical Society • Provided by theNASA Astrophysics Data System 2 Numerical resultsfortheglassplate(a=0*25).—Thetotalcorrectionof The correctionoftheoff-axis angledueonlytostretchingoftheplate isgiven In eachofTable I,II,IIIthemaximum possibleerroris± 0*0005. The correctionoftheposition angleisgivensimilarlyby8topositionangle Table V 15