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001 9910706590803321
005 20171114105131.0
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035   $a(OCoLC)1011356298
035   $a(EXLCZ)995470000002456535
100   $a20171113j200102    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSupersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system /$fJ.R. DeBonis and C.J. Trefny
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dFebruary 2001.
215   $a1 online resource (18 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210567
300   $a"February 2001."
300   $a"Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
320   $aIncludes bibliographical references (page 5).
517 3 $aSupersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion system
606   $aAir breathing boosters$2nasat
606   $aHypersonic speed$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aWind tunnel tests$2nasat
606   $aPropulsion$2nasat
606   $aPressure distribution$2nasat
615  7$aAir breathing boosters.
615  7$aHypersonic speed.
615  7$aComputational fluid dynamics.
615  7$aWind tunnel tests.
615  7$aPropulsion.
615  7$aPressure distribution.
700   $aDeBonis$b James R.$01387413
702   $aTrefny$b Charles J.
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706590803321
996   $aSupersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system$93444583
997   $aUNINA