LEADER 02067nam  2200589I  450 
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100   $a20130208d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFlight test results on the stability and control of the F-15 Quiet Spike aircraft /$fCheng M. Moua [and three others]
210  1$aEdwards, CA :$cNational Aeronautics and, Space Administration, Dryden Flight Research Center,$d[2012]
215   $a1 online resource (41 pages) $ccolor illustrations
225 1 $a[NASA technical memorandum] ;$vNASA/TM 2012-215978
300   $aTitle from title screen (viewed Feb. 8, 2013).
300   $a"February 2012."
320   $aIncludes bibliographical references (page 15-16).
606   $aF-15 aircraft$2nasat
606   $aFlight tests$2nasat
606   $aAircraft control$2nasat
606   $aAircraft stability$2nasat
606   $aSupersonic flight$2nasat
606   $aSonic booms$2nasat
606   $aFuselages$2nasat
606   $aNoses (forebodies)$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aFlight control$2nasat
615  7$aF-15 aircraft.
615  7$aFlight tests.
615  7$aAircraft control.
615  7$aAircraft stability.
615  7$aSupersonic flight.
615  7$aSonic booms.
615  7$aFuselages.
615  7$aNoses (forebodies)
615  7$aComputational fluid dynamics.
615  7$aFlight control.
700   $aMoua$b Cheng M.$01407032
712 02$aHugh L. Dryden Flight Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702345403321
996   $aFlight test results on the stability and control of the F-15 Quiet Spike aircraft$93487373
997   $aUNINA

LEADER 01876oam  2200541I  450 
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035   $a(EXLCZ)995470000002472849
100   $a20180705j198605    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDesign of fuselage shapes for natural laminar flow /$fS.S. Dodbele, C.P. van Dam, P.M.H.W. Vijgen
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dMarch 1986.
215   $a1 online resource (vii, 34 pages) $cillustrations
225 1 $aNASA/CR ;$v3970
300   $a"March 1986."
300   $a"Vigyan Research Associates, Inc."
320   $aIncludes bibliographical references (pages 14-15).
606   $aAircraft design$2nasat
606   $aAerodynamic configurations$2nasat
606   $aFuselages$2nasat
606   $aLaminar flow$2nasat
606   $aBoundary layers$2nasat
615  7$aAircraft design.
615  7$aAerodynamic configurations.
615  7$aFuselages.
615  7$aLaminar flow.
615  7$aBoundary layers.
700   $aDodbele$b S. S.$01417577
702   $aVan Dam$b C. P$g(Cornelis P.),$f1954-
702   $aVijgen$b Paul M. H. W.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aVigyan Research Associates.
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
801  2$bMERUC
801  2$bGPO
906   $aBOOK
912   $a9910709739903321
996   $aDesign of fuselage shapes for natural laminar flow$93526436
997   $aUNINA