02628oam 2200745I 450 991070961670332120180612110006.0(CKB)5470000002472073(OCoLC)761382490(OCoLC)995470000002472073(EXLCZ)99547000000247207320111115j198501 ua 0engurun||||a|a||txtrdacontentcrdamediacrrdacarrierAerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes /Robert J. Nowak, Cindy W. Albertson, and L. Roane HuntWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch,January 1985.1 online resource (87 pages) illustrationsNASA/TP ;2345"January 1985."Prepared at Langley Research Center.Includes bibliographical references (pages 19-21).Flow distributionnasatConesnasatAerodynamic heatingnasatBoundary layer transitionnasatTurbulent boundary layernasatAngle of attack (Aerodynamics)Noses (Aircraft)Reynolds numberAerothermodynamicsAerothermodynamicsfastAngle of attack (Aerodynamics)fastNoses (Aircraft)fastReynolds numberfastFlow distribution.Cones.Aerodynamic heating.Boundary layer transition.Turbulent boundary layer.Angle of attack (Aerodynamics)Noses (Aircraft)Reynolds number.Aerothermodynamics.Aerothermodynamics.Angle of attack (Aerodynamics)Noses (Aircraft)Reynolds number.Nowak Robert J.1401795Albertson Cindy W.Hunt L. Roane(Lewis Roane),United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCFOCLCOOCLCQGPOBOOK9910709616703321Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes3470994UNINA