01840oam 2200493I 450 991071405060332120201113125601.0(CKB)5470000002507140(OCoLC)761487580(EXLCZ)99547000000250714020111115j196810 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierFlow-field properties near an arrow-wing--body model at Mach numbers of 1.60, 2.36, and 2.96 /by Robert L. Weirich and Walter A. VahlWashington, D.C. :National Aeronautics and Space Administration,October 1968.1 online resource (135 pages) illustrationsNASA technical note ;TN D-4809"October 1968."Includes bibliographical references (page 12).Supersonic wind tunnelsTestingSupersonic planesDesign and constructionSupersonic planesTestingSupersonic planesDesign and constructionfastSupersonic wind tunnelsTestingfastSupersonic wind tunnelsTesting.Supersonic planesDesign and construction.Supersonic planesTesting.Supersonic planesDesign and construction.Supersonic wind tunnelsTesting.Weirich Robert L.1398246Vahl Walter A.United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCFGPOBOOK9910714050603321Flow-field properties near an arrow-wing--body model at Mach numbers of 1.60, 2.36, and 2.963461227UNINA