02066oam 2200541I 450 991071389290332120200820144110.0(CKB)5470000002504761(OCoLC)1100474486(EXLCZ)99547000000250476120190508d1953 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 /by Paige B. Burbank and Robert W. ByrneWashington, [D.C.] :National Advisory Committee for Aeronautics,1953.1 online resource (37 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 2921"April 1953."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 11).NozzlesFluid dynamicsMach numberSupersonic nozzlesDesign and constructionMach numberfastNozzlesFluid dynamicsfastSupersonic nozzlesDesign and constructionfastNozzlesFluid dynamics.Mach number.Supersonic nozzlesDesign and construction.Mach number.NozzlesFluid dynamics.Supersonic nozzlesDesign and construction.Burbank Paige B.1421146Byrne Robert W.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910713892903321The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.753541659UNINA