LEADER 01535nam  2200445Ka 450 
001 9910697709503321
005 20081120134301.0
035   $a(CKB)5470000002391882
035   $a(OCoLC)275189433
035   $a(EXLCZ)995470000002391882
100   $a20081120d1985      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNoise constraints effecting optimal propeller designs$b[electronic resource] /$fChristopher J. Miller and John P. Sullivan
210  1$a[Wasington, D.C.] :$cNational Aeronautics and Space Administration,$d[1985]
215   $a7 pages, 6 unnumbered pages $cdigital, PDF file
225 1 $aNASA technical memorandum ;$v86967
606   $aPropeller blades$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aAerodynamic noise$2nasat
606   $aAircraft design$2nasat
606   $aNoise reduction$2nasat
606   $aOptimization$2nasat
615  7$aPropeller blades.
615  7$aAerodynamic characteristics.
615  7$aAerodynamic noise.
615  7$aAircraft design.
615  7$aNoise reduction.
615  7$aOptimization.
700   $aMiller$b C. J$g(Christopher J.)$01415910
701   $aSullivan$b John P$0921953
712 02$aUnited States.$bNational Aeronautics and Space Administration.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697709503321
996   $aNoise constraints effecting optimal propeller designs$93519413
997   $aUNINA