02288oam 2200625 450 991070979590332120180615080000.0(CKB)5470000002472283(OCoLC)785231972(EXLCZ)99547000000247228320120408j198506 ua 0engurbn||||||abptxtrdacontentcrdamediacrrdacarrierWind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter /Arthur E. Phelps III and John D. BerryWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch,June 1985.1 online resource (73 pages) illustrationsNASA/TP ;2420AVSCOM technical report ;85-B-2"June 1985."Includes bibliographical references (page 14).Scale modelsnasatAerodynamic characteristicsnasatAerodynamic configurationsnasatWind tunnel testsnasatHelicopter performancenasatMilitary helicoptersTestingMilitary helicoptersStabilityMilitary helicoptersTestingfastScale models.Aerodynamic characteristics.Aerodynamic configurations.Wind tunnel tests.Helicopter performance.Military helicoptersTesting.Military helicoptersStability.Military helicoptersTesting.Phelps Arthur E.1415979Berry John D.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,United States.Army Aviation Systems Command.Langley Research Center.OCLCEOCLCEOCLCQOCLCOOCLCQOCLCFGPOBOOK9910709795903321Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter3519710UNINA