LEADER 01926nam  2200421 n 450 
001 996386629603316
005 20200824121450.0
035   $a(CKB)1000000000621343
035   $a(EEBO)2240898965
035   $a(UnM)99839648
035   $a(EXLCZ)991000000000621343
100   $a19901220d1603      uy             |
101 0 $aeng
135   $aurbn||||a|bb|
200 13$aAn ansvver to the first part of a certaine conference, concerning succession, published not long since vnder the name of R. Dolman$b[electronic resource]
210   $aAt London $cImprinted [by Eliot's Court Press, R. Bradock, P. Short, T. Snodham, R. Field, and J. Harrison] for Simon Waterson, and Cuthbert Burbie$d1603
215   $a[168] p
300   $aDedication signed: Io: Hayvvard.
300   $aA reply to: A conference about the next succession to the crowne of Ingland.
300   $a"Eliot's Court Press pr[inted]. piA, Bradock A-C, Short D-G, Snodham H-L, Field M-P, and Harrison Q-V"--STC.
300   $aSignatures: A⁴ ² A-V⁴.
300   $aThe first leaf is blank except for signature-mark "A".
300   $aQuires D-G are paginated 17-48.
300   $aSome copies have slip-cancels on F2r line 5, I2v lines 24,25, and I4r line 16.
300   $aReproduction of the original in the Henry E. Huntington Library and Art Gallery.
330   $aeebo-0113
606   $aKings and rulers$xSuccession$vEarly works to 1800
607   $aGreat Britain$xKings and rulers$xSuccession$vEarly works to 1800
615  0$aKings and rulers$xSuccession
700   $aHayward$b John$cSir,$f1564?-1627.$01001353
801  0$bCu-RivES
801  1$bCu-RivES
801  2$bCStRLIN
801  2$bWaOLN
906   $aBOOK
912   $a996386629603316
996   $aAn ansvver to the first part of a certaine conference, concerning succession, published not long since vnder the name of R. Dolman$92321133
997   $aUNISA

LEADER 01586oam  2200445   450 
001 9910716529303321
005 20210701112138.0
035   $a(CKB)5470000002522865
035   $a(OCoLC)890693636
035   $a(EXLCZ)995470000002522865
100   $a20140916j197212    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNumerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation /$fby Russell B. Sorrells and David S. Miller
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1972.
215   $a1 online resource (47 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7097
300   $a"December 1972."
320   $aIncludes bibliographical references (page 21).
606   $aAerodynamics$2nasat
606   $aCamber$2nasat
606   $aWings$2nasat
615  7$aAerodynamics.
615  7$aCamber.
615  7$aWings.
700   $aSorrells$b Russell B.$01414584
702   $aMiller$b David S$c(Of Langley Research Center),
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716529303321
996   $aNumerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation$93514307
997   $aUNINA