LEADER 01994oam  2200529   450 
001 9910713879903321
005 20200825134918.0
035   $a(CKB)5470000002504892
035   $a(OCoLC)1104148324
035   $a(EXLCZ)995470000002504892
100   $a20190610d1956      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAnalysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel /$fby Stanley H. Scher
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1956.
215   $a1 online resource (54 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3611
300   $a"April 1956."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 22).
606   $aAirplanes$xTesting
606   $aSpin (Aerodynamics)
606   $aWind tunnel testing
606   $aAirplanes$xTesting$2fast
606   $aSpin (Aerodynamics)$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xTesting.
615  0$aSpin (Aerodynamics)
615  0$aWind tunnel testing.
615  7$aAirplanes$xTesting.
615  7$aSpin (Aerodynamics)
615  7$aWind tunnel testing.
700   $aScher$b Stanley H.$01416899
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713879903321
996   $aAnalysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel$93523777
997   $aUNINA