LEADER 01628oam  2200457   450 
001 9910713422203321
005 20200501140716.0
035   $a(CKB)5470000002501434
035   $a(OCoLC)1121049797
035   $a(EXLCZ)995470000002501434
100   $a20190926d1924      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNote on the relative effect of the dihedral and the sweep back of airplane wings /$fby Max M. Munk
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1924.
215   $a1 online resource (4 pages)
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 177
300   $a"January, 1924."
300   $aNo Federal Depository Library Program (FDLP) item number.
606   $aAirplanes$xWings, Swept-back
606   $aAirplanes$xDihedral wings
606   $aAirplanes$xDihedral wings$2fast
606   $aAirplanes$xWings, Swept-back$2fast
615  0$aAirplanes$xWings, Swept-back.
615  0$aAirplanes$xDihedral wings.
615  7$aAirplanes$xDihedral wings.
615  7$aAirplanes$xWings, Swept-back.
700   $aMunk$b Max M$g(Max Michael),$f1890-$01386130
712 02$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   $a9910713422203321
996   $aNote on the relative effect of the dihedral and the sweep back of airplane wings$93434766
997   $aUNINA