LEADER 01701oam  2200481   450 
001 9910717169703321
005 20220210080858.0
035   $a(CKB)5470000002528517
035   $a(OCoLC)1154792312
035   $a(EXLCZ)995470000002528517
100   $a20200519d1939      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn approximate spin design criterion for monoplanes /$fby Oscar Seidman and Charles J. Donlan
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939.
215   $a1 online resource (7 pages, 4 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 711
300   $a"June 1939."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 7).
606   $aAirplanes$xDesign and construction
606   $aSpin (Aerodynamics)
606   $aAirplanes$xDesign and construction$2fast
606   $aSpin (Aerodynamics)$2fast
615  0$aAirplanes$xDesign and construction.
615  0$aSpin (Aerodynamics)
615  7$aAirplanes$xDesign and construction.
615  7$aSpin (Aerodynamics)
700   $aSeidman$b Oscar$01405963
702   $aDonlan$b Charles J.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910717169703321
996   $aAn approximate spin design criterion for monoplanes$93548574
997   $aUNINA