Magnus effect over finned projectiles

Journal of Spacecraft and Rockets

Volumn 38, Issue 4, 2001, Pages 542-549

  Pechier, Marc ^a   Guillen, Philippe ^a   Cayzac, Roxan ^b  

^a ONERA   (France)

^b Nexter Munitions   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW TURBOMACHINERY; BOUNDARY LAYERS; ELECTRIC DISTORTION; FINS (HEAT EXCHANGE); LINEARIZATION; STEADY FLOW; TURBULENT FLOW; VORTEX FLOW;

FINNED PROJECTILES; MAGNUS EFFECT;

PROJECTILES;

EID: 0035390391     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3714     Document Type: Article

References (14)

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7. Lower-upper implicit scheme with multiple grids for the Euler equations
8. Implicit schemes and LU decomposition
9. Time accuracy and the use of implicit methods
10. Aerodynamics of body tail projectiles, wind tunnel measurements and predictions of magnus coefficients at Mach number 4.3
11. Leeward flow over delta wings at supersonic speeds