LEADER 02304oam  2200601I  450 
001 9910713887703321
005 20200824084829.0
035   $a(CKB)5470000002504813
035   $a(OCoLC)1104148279
035   $a(EXLCZ)995470000002504813
100   $a20190610d1954      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180° /$fby H. Clyde McLemore and Michael D. Cannon
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1954.
215   $a1 online resource (62 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3228
300   $a"June 1954."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 15).
517 3 $aAerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 degrees to 180 degrees
606   $aAngle of attack (Aerodynamics)
606   $aMathematical analysis
606   $aPropellers, Aerial$xTesting
606   $aWind tunnel testing
606   $aAngle of attack (Aerodynamics)$2fast
606   $aMathematical analysis$2fast
606   $aPropellers, Aerial$xTesting$2fast
606   $aWind tunnel testing$2fast
615  0$aAngle of attack (Aerodynamics)
615  0$aMathematical analysis.
615  0$aPropellers, Aerial$xTesting.
615  0$aWind tunnel testing.
615  7$aAngle of attack (Aerodynamics)
615  7$aMathematical analysis.
615  7$aPropellers, Aerial$xTesting.
615  7$aWind tunnel testing.
700   $aMcLemore$b H. Clyde$01404416
702   $aCannon$b Michael D.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713887703321
996   $aAerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180$93478944
997   $aUNINA