Proj
J-GLOBAL ID:200904004633418793  Research Project code:9800033986 Update date:Nov. 22, 1996

Study on turbulent flow transition characteristics in compressive flow of obtuse conical missile

鈍頭コーン状飛行体での圧縮性流れでの乱流遷移特性
Study period:1993 - 1993
Organization (1):
Investigating Researcher (1):
Keywords (8):
blunt ,  flying ,  compressible ,  turbulent ,  transitional ,  spacecraft ,  reentry ,  supersonic
Research program: Ordinary Research
Ministry with control over the research :
Ministry of Education, Culture, Sports, Science and Technology

Return to Previous Page