Large-scale Static Investigation of Circulation-control-wing Concepts Applied to Upper Surface-blowing Aircraft
National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987 - Air flow - 60 pages
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aircraft data system Airfoil airplane Ames Research Center analog signals axial and normal axial force baseline configuration Bethesda blowing momentum blown system calculated CCW assembly CCW Design CCW device CCW trailing edge CCW trailing-edge CCW/USB concept CCW/USB system circular arc configuration CIRCULATION-CONTROL-WING comparison CONFIG cruise drag David Taylor Naval Development Center DTNSRDC end plate engine exhaust entrain FENCE flexure beam horizontal force improvements in.-diam increased thrust installed jet sheet lb/ft RUNS CARTS left inboard engine lift lift force load pads mass flow measured model-scale Moffett Field mVj/bj NASA Naval Ship Research normal forces nozzle parameters PCCW performance Phase I baseline Phase I fig plenum POWER SETTING pressure produced psig lb/sec CARTS QSRA radius ratio reduced resultant thrust shown in figure smaller slot height ST0L Static thrust turning STOL Taylor Naval Ship temperature thrust deflection thrust level thrust turning angle turbofan USB flap vertical force vortex