LEADER 01802oam  2200517   450 
001 9910717101803321
005 20220224115343.0
035   $a(CKB)5470000002529203
035   $a(OCoLC)1158388804
035   $a(EXLCZ)995470000002529203
100   $a20200615d1940      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aDrag determinations of the forward component of a tricycle landing gear /$fby Hubert N. Harmon
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1940.
215   $a1 online resource (7 pages, 20 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 788
300   $a"December 1940."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 5).
606   $aAirplanes$xLanding gear
606   $aDrag (Aerodynamics)
606   $aWind tunnel testing
606   $aAirplanes$xLanding gear$2fast
606   $aDrag (Aerodynamics)$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xLanding gear.
615  0$aDrag (Aerodynamics)
615  0$aWind tunnel testing.
615  7$aAirplanes$xLanding gear.
615  7$aDrag (Aerodynamics)
615  7$aWind tunnel testing.
700   $aHarmon$b Hubert N.$01400989
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910717101803321
996   $aDrag determinations of the forward component of a tricycle landing gear$93468936
997   $aUNINA