Aerodynamic analysis of a spinning missile with dithering canards

Journal of Spacecraft and Rockets

Volumn 41, Issue 5, 2004, Pages 726-734

  Nygaard, Tor A ^a,c   Meakin, Robert L ^b,d  

^a ELORET CORPORATION   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

^c Army/NASA Rotorcraft Division ^*  (United States)

^d Army/NASA Rotorcraft Division   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; MISSILES; PROBLEM SOLVING; REYNOLDS NUMBER;

AXIAL FORCE; GRID POINTS; ROLLING MOMENTS; SPINNING MISSILE;

AERODYNAMICS;

EID: 7544244133     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.13075     Document Type: Article

References (11)

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