Transonic Shock-Turbulent Boundary Layer Interactions on Spinning Axisymmetric Bodies at Zero Angle of Attack

Author(s):  
George R. Inger

1982 ◽  
Vol 104 (4) ◽  
pp. 529-536 ◽  
Author(s):  
S. Taniguchi ◽  
H. Sakamoto ◽  
M. Arie

Measurements were made of the circumferential pressure distributions around two cylinders of finite height h and diameter d, spaced a distance s apart and vertically immersed in a turbulent boundary layer. The angle of attack φ and the dimensionless spacing s/d were varied. Drag and lift characteristics of both cylinders were classified into three regions divided by two zero-lift lines, namely 0 ≲ φ ≲ 30 deg, 30 ≲ φ ≲ 120 deg, and 120 ≲ φ ≲ 180 deg, in which interference between the two cylinders was found to be almost negligible for s/d ≳ 4.0, except for an influence in the wake region of the upstream cylinder.



AIAA Journal ◽  
1978 ◽  
Vol 16 (7) ◽  
pp. 761-763 ◽  
Author(s):  
Dominique Aymer de la Chevalerie ◽  
Roger M. F. Leblanc




1976 ◽  
Vol 27 (2) ◽  
pp. 87-98 ◽  
Author(s):  
J L Stollery

SummaryComparisons are made between some measurements of skin friction and heat transfer over five axisymmetric bodies and the predictions of a simple theory. The development of the theory is outlined and explicit expressions obtained for all the gross turbulent boundary-layer characteristics (δ*,θ,H,Cf and St).





Sign in / Sign up

Export Citation Format

Share Document