02181oam 2200565I 450 991070702610332120160330152348.0(CKB)5470000002461229(OCoLC)755287619(EXLCZ)99547000000246122920111002j199708 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFlight demonstration of a shock location sensor using constant voltage hot-film anemometry /Timothy R. Moes, Garimella R. Sarma and Siva M. Mangalam[Washington, D.C.] :National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,August 1997.1 online resource (25 pages) illustrationsNASA technical memorandum ;4806Title from title screen (viewed March 30, 2016)."August 1997.""Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.Includes bibliographical references (page 25).Transonic speednasatLeading edgesnasatLaminar boundary layernasatHot-film anemometersnasatAirfoilsnasatTransonic speed.Leading edges.Laminar boundary layer.Hot-film anemometers.Airfoils.Moes Timothy R.1386042Sarma Garimella R.Mangalam Siva M.NASA Dryden Flight Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Program,United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCFOCLCOGPOBOOK9910707026103321Flight demonstration of a shock location sensor using constant voltage hot-film anemometry3522591UNINA