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100   $a20011207d1996----km-y0itay0103----ba
101   $aeng
102   $aUS
105   $a||||||||001yy
200 1 $aQuadratics$fRichard A. Mollin
210   $aBoca Raton$cCRC$dc1996
215   $aXX, 387 p$d24 cm
225 2 $aDiscrete mathematical and its applications
410   $12001$aDiscrete mathematical and its applications
606 0 $aEquazioni di 2. grado
676   $a512.7
700  1$aMOLLIN,$bRichard A.$065944
801  0$aIT$bsalbc$gISBD
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996   $aQuadratics$9924602
997   $aUNISA

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101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStatic internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ?/$fLaurence D. Leavitt
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dFebruary 1985.
215   $a1 online resource (66 pages) $cillustrations
225 1 $aNASA/TP ;$v2391
300   $a"February 1985."
320   $aIncludes bibliographical references (pages 7-8).
606   $aConvergent$2nasat
606   $aThrust vector control$2nasat
606   $aWind tunnel tests$2nasat
606   $aNozzle flow$2nasat
606   $aTransonic wind tunnels$2nasat
615  7$aConvergent.
615  7$aThrust vector control.
615  7$aWind tunnel tests.
615  7$aNozzle flow.
615  7$aTransonic wind tunnels.
700   $aLeavitt$b Laurence D.$01394871
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910709978403321
996   $aStatic internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ?$93452729
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