scholarly journals A kinetic study of the hypersonic flow past the leading edge of a flat plate

1970 ◽  
Author(s):  
W. CHOW ◽  
R. EL-ASSAR
Keyword(s):  
Kinetic Study ◽  
Flat Plate ◽  
Hypersonic Flow ◽  
Leading Edge ◽  
Flow Past

Hypersonic Flow Near the Leading Edge of a Flat Plate

1960 ◽  
Vol 3 (1) ◽  
pp. 140 ◽  
Author(s):  
H. T. Nagamatsu ◽  
T. Y. Li
Keyword(s):  
Flat Plate ◽  
Hypersonic Flow ◽  
Leading Edge

Laminar incompressible flow past a semi-infinite flat plate

1967 ◽  
Vol 27 (4) ◽  
pp. 691-704 ◽  
Author(s):  
R. T. Davis
Keyword(s):  
Flat Plate ◽  
Incompressible Flow ◽  
Stokes Equations ◽  
Leading Edge ◽  
Navier Stokes ◽  
Local Similarity ◽  
Approximate Methods ◽  
Navier Stokes Equations ◽  
Flow Past

Laminar incompressible flow past a semi-infinite flat plate is examined by using the method of series truncation (or local similarity) on the full Navier-Stokes equations. The first and second truncations are calculated at points on the plate away from the leading edge, while only the first truncation is calculated at the leading edge. The solutions are compared with the results from other approximate methods.

Hypersonic Slip Flow past the Leading Edge of a Flat Plate

AIAA Journal ◽  
1966 ◽  
Vol 4 (11) ◽  
pp. 2062-2063 ◽  
Author(s):  
W. L. CHOW
Keyword(s):  
Flat Plate ◽  
Slip Flow ◽  
Leading Edge ◽  
Flow Past

scholarly journals About the features of hypersonic flow past a yawed plate

2019 ◽  
Vol 487 (1) ◽  
pp. 24-27
Author(s):  
G. N. Dudin ◽  
V. Ya. Neyland
Keyword(s):  
Hypersonic Flow ◽  
Strong Interaction ◽  
Leading Edge ◽  
Transverse Coordinate ◽  
Trailing Edge ◽  
The Third ◽  
Flow Past ◽  
Flow Functions

The flow around the yawed plate in the regime of strong interaction is considered in the case when the pressure at its trailing edge is not constant, but changes along the transverse coordinate. It is shown that in the case of large transverse gradients of the induced pressure, the type of expansions of flow functions in the vicinity of the leading edge changes significantly and the third term of the expansions should be taken into account.

Leading edge effect on rarefied hypersonic flow over a flat plate

1991 ◽  
Author(s):  
K. HEFFNER ◽  
L. GOTTESDIENER ◽  
A. CHPOUN ◽  
J. LENGRAND
Keyword(s):  
Flat Plate ◽  
Hypersonic Flow ◽  
Edge Effect ◽  
Leading Edge

scholarly journals Prandtl–Batchelor flow past a flat plate with a forward-facing flap

1984 ◽  
Vol 143 ◽  
pp. 351-365 ◽  
Author(s):  
P. G. Saffman ◽  
S. Tanveer
Keyword(s):  
Flat Plate ◽  
Leading Edge ◽  
Vortex Sheet ◽  
Inviscid Flow ◽  
The Body ◽  
Two Dimensional ◽  
Rear Edge ◽  
Flow Past ◽  
Range Of Values ◽  
Streamline Method

Two-dimensional steady inviscid flow past an inclined flat plate with a forward-facing flap attached to the rear edge is considered for the case when a vortex sheet separates from the leading edge of the flat plate and reattaches at the leading edge of the flap, with uniform vorticity distributed between the vortex sheet and the body. Solutions are found for a particular geometry and a range of values of the vorticity. The method used to calculate the flow is an extension of a free-streamline method widely used in cases where the velocity is a constant on the separating streamline.

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