| Record ID | marc_miami_univ_ohio/allbibs0087.out:6677851:1601 |
| Source | Miami University of Ohio |
| Download Link | /show-records/marc_miami_univ_ohio/allbibs0087.out:6677851:1601?format=raw |
LEADER: 01601nam 2200361 a 4500
001 ocm11853922
008 850327s1984 dcua tb f00010 eng d
040 $aGPO$cGPO
049 $aMIB*
074 $a0830-H-14
086 0 $aNAS 1.26:3825
086 0 $aNAS 1.26:3825
100 10 $aTaylor, Robert B.,$d1945-
245 10 $aHelicopter rotor blade design for minimum vibration /$cRobert B. Taylor
260 0 $aWashington, D.C. :$bNational Aeronautics and Space Administration, Scientific and Technical Information Branch ;$a[Springfield, Va. :$bFor sale by the National Technical Information Service],$c1984
300 $axvii, 127 p. :$bill. ;$c28 cm
440 0 $aNASA contractor report ;$v3825
440 0 $aAVSCOM technical report ;$v84-A-2
500 $a"United Technologies Research Center."
500 $aDistributed to depository libraries in microfiche
500 $a"October 1984"--Cover
500 $aSTAR category 05
504 $aIncludes bibliographical references
513 $aFinal report
536 $aAeromechanics Laboratory, U.S. Army Research and Technology Laboratories, Ames Research Center.$bNAS2-11025
650 0 $aRotors (Helicopters)
650 0 $aStability of helicopters
710 10 $aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch
710 20 $aUnited Technologies Research Center
710 20 $aAeromechanics Laboratory
907 $a.b21541504$b10-15-98$c11-13-94
998 $adoc$b11-13-94$cm$da$e-$feng$gdcu$h0$i1
945 $g1$j0$ldocsf$nrecd$o-$p$0.00$sf$t21$u0$v0$w0$x0$y.i25507540$z11-13-94