Numerical and experimental investigation on sloshing in rocket tanks with damping devices

Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference

Volumn 5, Issue , 2007, Pages 5296-5312

  Himeno, Takehiro ^a,d   Watanabe, Toshinori ^a,d   Nonaka, Satoshi ^b,d   Naruo, Yoshihiro ^b,d   Inatani, Yoshifumi ^b,d   Aoki, Hiroshi ^c,d  

^a UNIVERSITY OF TOKYO   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c Japan Aerospace Exploration Agency   (Japan)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DAMPING DEVICES; REUSABLE LAUNCH VEHICLES; ROCKET TANKS; SUB-SCALE MODELS;

COMPUTATIONAL FLUID DYNAMICS; FLIGHT SIMULATORS; FUEL SLOSHING; MISSILE LAUNCHING SYSTEMS; REUSABLE ROCKETS;

FUEL TANKS;

EID: 36749026274     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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