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100   $a20170202j199304    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental effects of wing location on wing-body pressures at supersonic speeds /$fJerry M. Allen and Carolyn B. Watson
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dApril 1993.
215   $a1 online resource (195 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4434
300   $a"April 1993" Report documentation page.
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 6).
606   $aAngle of attack$2nasat
606   $aBody-wing configurations$2nasat
606   $aFlow coefficients$2nasat
606   $aPressure distribution$2nasat
606   $aSupersonic flight$2nasat
606   $aSupersonic speed$2nasat
615  7$aAngle of attack.
615  7$aBody-wing configurations.
615  7$aFlow coefficients.
615  7$aPressure distribution.
615  7$aSupersonic flight.
615  7$aSupersonic speed.
700   $aAllen$b Jerry M.$01400290
702   $aWatson$b Carolyn B.
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707953503321
996   $aExperimental effects of wing location on wing-body pressures at supersonic speeds$93541323
997   $aUNINA