
Study on Reflected Pressure in a Shock Tunnel According to the Size of a Nozzle Throat
Author(s) -
Jong Kook Lee
Publication year - 2015
Publication title -
han-guk hanggong uju hakoeji/han'gug hang'gong u'ju haghoeji
Language(s) - English
Resource type - Journals
eISSN - 2287-6871
pISSN - 1225-1348
DOI - 10.5139/jksas.2015.43.6.479
Subject(s) - nozzle , stagnation temperature , shock tube , mechanics , stagnation pressure , shock (circulatory) , expansion tunnel , throat , discharge coefficient , flow (mathematics) , materials science , shock wave , stagnation point , mechanical engineering , engineering , physics , mach number , medicine , heat transfer , anatomy