Second order theory for steady or unsteady subsonic flow past slender lifting bodies of finite thickness

1968 ◽  
Author(s):  
J. REVELL
Keyword(s):  
Subsonic Flow ◽  
Finite Thickness ◽  
Order Theory ◽  
Second Order ◽  
Flow Past

Second-order theory for flow past oscillating foils.

AIAA Journal ◽  
1968 ◽  
Vol 6 (8) ◽  
pp. 1556-1562 ◽  
Author(s):  
C. F. CHEN ◽  
RICHARD A. WIRTZ
Keyword(s):  
Order Theory ◽  
Second Order ◽  
Flow Past ◽  
Oscillating Foils

scholarly journals Second-Order Theory on Wall Effect in Cavitating Flow past a Thin Jet-Flapped foil

1976 ◽  
Vol 19 (137) ◽  
pp. 1285-1293
Author(s):  
Teruhiko KIDA ◽  
Yoshihiro MIYAI
Keyword(s):  
Order Theory ◽  
Cavitating Flow ◽  
Second Order ◽  
Wall Effect ◽  
Flow Past

Numerical solutions for steady symmetric viscous flow past a parabolic cylinder in a uniform stream

1971 ◽  
Vol 50 (4) ◽  
pp. 801-814 ◽  
Author(s):  
S. C. R. Dennis ◽  
J. D. Walsh
Keyword(s):  
Skin Friction ◽  
Numerical Solutions ◽  
Order Theory ◽  
Second Order ◽  
Parabolic Cylinder ◽  
Symmetric Flow ◽  
Nose Radius ◽  
Flow Past ◽  
Theoretical Results ◽  
Uniform Stream

Numerical solutions are presented for steady two-dimensional symmetric flow past a parabolic cylinder in a uniform stream parallel to its axis. The solutions cover the range R = 0·25 to ∞, where R is the Reynolds number based on the nose radius of the cylinder. For large R, the calculated skin friction near the nose of the cylinder is compared with known theoretical results obtained from second-order boundary-layer theory. Some discrepancy is found to exist between the present calculations and the second-order theory. For small R, it is possible to obtain a reasonably consistent check with a recent theoretical prediction for the limit of the skin friction near the nose of the cylinder as R → 0.

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