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100   $a20110224j199211    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPressure distribution for the wing of the YAV-8B airplane: with and without pylons /$fEdwin J. Saltzman [and three others]
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dNovember 1992.
215   $a1 online resource (24 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4429
300   $a"November 1992" Report Documentation page.
300   $a"Performing organization: NASA Dryden Flight Research Facility"-- Report Documentation page.
320   $aIncludes bibliographical references (pages 12-13).
517   $aPressure distribution for the wing of the YAV-8B airplane
606   $aFighter aircraft$2nasat
606   $aFlow characteristics$2nasat
606   $aPressure distribution$2nasat
606   $aPylons$2nasat
606   $aSupercritical wings$2nasat
615  7$aFighter aircraft.
615  7$aFlow characteristics.
615  7$aPressure distribution.
615  7$aPylons.
615  7$aSupercritical wings.
700   $aSaltzman$b Edwin J.$01389623
712 02$aDryden Flight Research Facility.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
801  0$bSSN
801  1$bSSN
801  2$bGPO
906   $aBOOK
912   $a9910707954103321
996   $aPressure distribution for the wing of the YAV-8B airplane: with and without pylons$93441444
997   $aUNINA