01796oam 2200517I 450 991071503330332120201124085012.0(CKB)5470000002507673(OCoLC)761231836(EXLCZ)99547000000250767320111115j196809 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierDescriptions and operating parameters of a Mach 2 nozzle system for the Langley 11-inch ceramic-heated tunnel /by Kenneth SuttonWashington, D.C. :National Aeronautics and Space Administration,September 1968.1 online resource (67 pages) illustrationsNASA technical note ;TN D-4750"September 1968."Includes bibliographical references (pages 18-19).NozzlesTestingMach numberTestingHeat resistant materialsTestingHeat resistant materialsTestingfastNozzlesTestingfastNozzlesTesting.Mach numberTesting.Heat resistant materialsTesting.Heat resistant materialsTesting.NozzlesTesting.Sutton Kenneth1403502United States.National Aeronautics and Space Administration,Langley Research Center.OCLCEOCLCEOCLCQOCLCOOCLCQOCLCFGPOBOOK9910715033303321Descriptions and operating parameters of a Mach 2 nozzle system for the Langley 11-inch ceramic-heated tunnel3476358UNINA