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001 9910714075303321
005 20201106090117.0
035   $a(CKB)5470000002506917
035   $a(OCoLC)761067530
035   $a(EXLCZ)995470000002506917
100   $a20111115j196811    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted v-tail /$fby Richard J. Margason and Garl L. Gentry, Jr
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dNovember 1968.
215   $a1 online resource (179 pages) $cillustrations
225 1 $aNASA technical note ;$vNASA TN D-4856
300   $a"November1968."
320   $aIncludes bibliographical references (page 16).
606   $aShort take-off and landing aircraft
606   $aBoundary layer control
606   $aPropellers, Aerial
606   $aAirplanes$xTail surfaces
606   $aAerodynamics
606   $aAerodynamics$2fast
606   $aAirplanes$xTail surfaces$2fast
606   $aBoundary layer control$2fast
606   $aPropellers, Aerial$2fast
606   $aShort take-off and landing aircraft$2fast
615  0$aShort take-off and landing aircraft.
615  0$aBoundary layer control.
615  0$aPropellers, Aerial.
615  0$aAirplanes$xTail surfaces.
615  0$aAerodynamics.
615  7$aAerodynamics.
615  7$aAirplanes$xTail surfaces.
615  7$aBoundary layer control.
615  7$aPropellers, Aerial.
615  7$aShort take-off and landing aircraft.
700   $aMargason$b Richard J.$01170468
702   $aGentry$b Garl L.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910714075303321
996   $aAerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted v-tail$93457121
997   $aUNINA