LEADER 02664oam 2200661I 450 001 9910713876003321 005 20240125000055.0 035 $a(CKB)5470000002504931 035 $a(OCoLC)1100474461 035 $a(EXLCZ)995470000002504931 100 $a20190508d1956 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAerodynamic characteristics and flying qualities of a tailless triangular-wing airplane configuration as obtained from flights of rocket-propelled models at transonic and low supersonic speeds /$fby Grady L. Mitcham, Joseph E. Stevens, and Harry P. Norris 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1956. 215 $a1 online resource (57 pages) $cillustrations 225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3753 300 $a"November 1956." 300 $a"Supersedes recently declassified NACA Research Memorandum L9L07, 1950"--Page 1. 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 25). 606 $aAirplanes$xModels$xTesting 606 $aTailless airplanes 606 $aAirplanes$xHandling characteristics 606 $aAerodynamics, Supersonic 606 $aAerodynamics, Transonic 606 $aAerodynamics, Supersonic$2fast 606 $aAerodynamics, Transonic$2fast 606 $aAirplanes$xHandling characteristics$2fast 606 $aAirplanes$xModels$xTesting$2fast 606 $aTailless airplanes$2fast 615 0$aAirplanes$xModels$xTesting. 615 0$aTailless airplanes. 615 0$aAirplanes$xHandling characteristics. 615 0$aAerodynamics, Supersonic. 615 0$aAerodynamics, Transonic. 615 7$aAerodynamics, Supersonic. 615 7$aAerodynamics, Transonic. 615 7$aAirplanes$xHandling characteristics. 615 7$aAirplanes$xModels$xTesting. 615 7$aTailless airplanes. 700 $aMitcham$b Grady L.$01410904 702 $aStevens$b Joseph E. 702 $aNorris$b Harry P. 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bCOP 801 2$bTRAAL 801 2$bGPO 906 $aBOOK 912 $a9910713876003321 996 $aAerodynamic characteristics and flying qualities of a tailless triangular-wing airplane configuration as obtained from flights of rocket-propelled models at transonic and low supersonic speeds$93500704 997 $aUNINA