01178nam a2200313 i 450099100082811970753620020507174115.0980410s1996 uk ||| | eng 0582299640b1076284x-39ule_instLE01302927ExLDip.to Matematicaeng537.6AMS 47A40AMS 58G37AMS 78A25Serbest, A. H.535170Direct and inverse electromagnetic scattering /A. H. Serbest, and S. R. Cloude, editorsHarlow :Longman ; Reading, Mass. : Addison Wesley Longman,1996275 p. :ill. ;25 cm.Pitman research notes in mathematics series, ISSN 02693674 ;361Electromagnetic waves-ScatteringCongressesCloude, Shane.b1076284x23-02-1728-06-02991000828119707536LE013 78-XX SER11 (1996)12013000097527le013-E0.00-l- 00000.i1085828328-06-02Direct and inverse electromagnetic scattering923311UNISALENTOle01301-01-98ma -enguk 0102066oam 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