LEADER 02045oam  2200613   450 
001 9910716550903321
005 20210623132915.0
035   $a(CKB)5470000002522647
035   $a(OCoLC)20643001$z(OCoLC)760999383$z(OCoLC)867807810
035   $a(EXLCZ)995470000002522647
100   $a19891113j197212    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTests of a mixed compression axisymmetric inlet with large transonic mass flow at Mach numbers 0.6 to 2.65 /$fby Donald B. Smeltzer and Norman E. Sorensen
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dDecember 1972.
215   $a1 online resource (v, 183 pages) $cillustrations
225 1 $aNASA/TN ;$vD-6971
300   $a"December 1972."
320   $aIncludes bibliographical references (page 26).
606   $aJet engines$2nasat
606   $aMach number$2nasat
606   $aPropulsion$2nasat
606   $aJet engines$xAir intakes
606   $aAerodynamics, Transonic
606   $aAerodynamics, Transonic$2fast
606   $aJet engines$xAir intakes$2fast
615  7$aJet engines.
615  7$aMach number.
615  7$aPropulsion.
615  0$aJet engines$xAir intakes.
615  0$aAerodynamics, Transonic.
615  7$aAerodynamics, Transonic.
615  7$aJet engines$xAir intakes.
700   $aSmeltzer$b Donald B.$01409446
702   $aSorensen$b Norman E.$f1930-
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aAmes Research Center.
801  0$bABC
801  1$bABC
801  2$bOCL
801  2$bAD#
801  2$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716550903321
996   $aTests of a mixed compression axisymmetric inlet with large transonic mass flow at Mach numbers 0.6 to 2.65$93495893
997   $aUNINA