Reynolds number effects on cone forebody side force

38th AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2008, Pages

  Meng, Xuanshi ^a   Qiao, Zhide ^a   Gao, Chao ^a   Luo, Shijun ^b   Liu, Feng ^b  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^b University of California at Irvine   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; BOUNDARY LAYERS; WIND TUNNELS;

CIRCULAR CONES; COMPLETE COVERAGES; CYLINDER MODEL; FREE STREAM; LOW-SPEED WIND TUNNEL; REYNOLDS NUMBER EFFECT; SEMI-APEX ANGLES; SQUARE WAVES;

REYNOLDS NUMBER;

EID: 78049504693     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-4303     Document Type: Conference Paper

References (14)

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14. Keener, E., Chapman, G., Cohen, L., and Taleghani, J., "Side forces on Forebodies at high angles of attack and Mach numbers from 0.1 to 0.7: two tangent ogives, paraboloid and cone," NASA TM X-3438, Feb. 1977.