02021oam 2200577Ka 450 991069899500332120090610112452.0(CKB)5470000002397921(OCoLC)384172382(EXLCZ)99547000000239792120090610d1989 ua 0engtxtrdacontentcrdamediacrrdacarrierFeasibility and benefits of laminar flow control on supersonic cruise airplanes[electronic resource] /A.G. Powell, S. Agrawal, T. R. LaceyHampton, Va. :National Aeronautics and Space Administration, Langley Research Center,[1989]1 volumeNASA contractor report ;181817Title from title screen (viewed Jun. 9, 2009)Aerodynamic configurationsnasatBoundary layer controlnasatBoundary layer stabilitynasatFeasibility analysisnasatFighter aircraftnasatLaminar boundary layernasatLaminar flownasatSupersonic aircraftnasatSupersonic cruise aircraft researchnasatSupersonic transportsnasatAerodynamic configurations.Boundary layer control.Boundary layer stability.Feasibility analysis.Fighter aircraft.Laminar boundary layer.Laminar flow.Supersonic aircraft.Supersonic cruise aircraft research.Supersonic transports.Powell A. G1389264Agrawal Sudhir515084Lacey T. R1389265Langley Research Center.GPOGPOGPOBOOK9910698995003321Feasibility and benefits of laminar flow control on supersonic cruise airplanes3440557UNINA