01580oam 2200445I 450 991071409000332120201211101825.0(CKB)5470000002506769(OCoLC)890696419(EXLCZ)99547000000250676920140916j196903 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierExperimental pressure distributions on a 120° cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0° to 20° /by Robert L. Stallings and Dorothy H. TudorWashington, D.C. :National Aeronautics and Space Administration,March 1969.1 online resource (76 pages) illustrationsNASA technical note ;TN D-5054"March 1969."Includes bibliographical references (page 13).AerodynamicsnasatMach numbernasatPressure distributionnasatAerodynamics.Mach number.Pressure distribution.Stallings Robert L.1396665Tudor Dorothy H.United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQCOPGPOBOOK9910714090003321Experimental pressure distributions on a 120° cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0° to 203457106UNINA