Application of BCFD unstructured grid solver to simulation of micro-ramp control of shock/boundary layer interactions

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2007, Pages 315-326

  Shinn, A F ^a,c,d   Vanka, S P ^a,d,e   Mani, M ^b,d   Dorgan, A ^b,d   Michal, T ^b,d  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^b BOEING COMPANY   (United States)

^c Aerospace Engineering Department

^d AIAA   (United States)

^e Mechanical Science and Engineering Department

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPUTER SIMULATION; FLOW OF FLUIDS; MACH NUMBER; NAVIER STOKES EQUATIONS; PERTURBATION TECHNIQUES; SHOCK WAVES;

BCFD UNSTRUCTURED GRID SOLVER; IMPLICIT TIME-MARCHING METHOD; MICRO-RAMP CONTROL; OBLIQUE SHOCK WAVE;

BOUNDARY LAYERS;

EID: 35648994815     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-3914     Document Type: Conference Paper

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