LEADER 02675oam  2200781   450 
001 9910709724803321
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035   $a(CKB)5470000002473001
035   $a(OCoLC)761197631
035   $a(OCoLC)995470000002473001
035   $a(EXLCZ)995470000002473001
100   $a20111115j198604    ua             0
101 0 $aeng
135   $aurun||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStatic investigation of two STOL nozzle concepts with pitch thrust-vectoring capability /$fMary L. Mason and James R. Burley II
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dApril 1986.
215   $a1 online resource (54 pages) $cillustrations
225 1 $aNASA/TP ;$v2559
300   $a"April 1986."
320   $aIncludes bibliographical references (pages 13-14).
606   $aNozzle geometry$2nasat
606   $aStatic tests$2nasat
606   $aNozzle thrust coefficients$2nasat
606   $aAxisymmetric flow$2nasat
606   $aAfterburning$2nasat
606   $aJet nozzles$xTesting
606   $aAirplanes$xMotors$xThrust
606   $aPitching (Aerodynamics)
606   $aShort take-off and landing aircraft
606   $aAirplanes$xMotors$xThrust$2fast
606   $aJet nozzles$xTesting$2fast
606   $aPitching (Aerodynamics)$2fast
606   $aShort take-off and landing aircraft$2fast
608   $aOnline resources.
615  7$aNozzle geometry.
615  7$aStatic tests.
615  7$aNozzle thrust coefficients.
615  7$aAxisymmetric flow.
615  7$aAfterburning.
615  0$aJet nozzles$xTesting.
615  0$aAirplanes$xMotors$xThrust.
615  0$aPitching (Aerodynamics)
615  0$aShort take-off and landing aircraft.
615  7$aAirplanes$xMotors$xThrust.
615  7$aJet nozzles$xTesting.
615  7$aPitching (Aerodynamics)
615  7$aShort take-off and landing aircraft.
700   $aMason$b Mary L.$01407755
702   $aBurley$b James R.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
801  2$bMERUC
801  2$bGPO
906   $aBOOK
912   $a9910709724803321
996   $aStatic investigation of two STOL nozzle concepts with pitch thrust-vectoring capability$93506423
997   $aUNINA