LEADER 02100oam  2200637Ia 450 
001 9910702197403321
005 20120910100541.0
035   $a(CKB)5470000002424160
035   $a(OCoLC)809536291
035   $a(EXLCZ)995470000002424160
100   $a20120910g19851985  ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStudy for prediction of rotor/wake/fuselage interference$b[electronic resource] /$fD. R. Clark, B. Maskew
210   $aRedmond, WA $cAnalytical Methods, Inc. ;$aMoffett Field, Calif $cNational Aeronautics and Space Administration, Ames Research Center$d[1985]
215   $a1 online resource (2 volumes) $cillustrations
225 1 $aNASA contractor report ;$v177340
300   $aTitle from title screen (viewed on Sept. 10, 2012).
300   $a"March 1985"--pt. 1.
300   $a"November 1983"--pt. 2.
320   $aIncludes bibliographical references.
327   $apt. I. Technical report. -- pt. II. Program users guide.
606   $aAerodynamic interference$2nasat
606   $aAir flow$2nasat
606   $aAircraft configurations$2nasat
606   $aFuselages$2nasat
606   $aHelicopter wakes$2nasat
606   $aHelicopters$2nasat
606   $aLoads (forces)$2nasat
606   $aRotary wings$2nasat
606   $aRotor aerodynamics$2nasat
606   $aVortices$2nasat
615  7$aAerodynamic interference.
615  7$aAir flow.
615  7$aAircraft configurations.
615  7$aFuselages.
615  7$aHelicopter wakes.
615  7$aHelicopters.
615  7$aLoads (forces)
615  7$aRotary wings.
615  7$aRotor aerodynamics.
615  7$aVortices.
700   $aClark$b D. R$01407916
701   $aMaskew$b B$01388303
712 02$aAnalytical Methods, Inc.
712 02$aAmes Research Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910702197403321
996   $aStudy for prediction of rotor$93490444
997   $aUNINA