Chordwise and compressibility corrections for arbitrary planform slender wings

AIAA Journal ◽  
1982 ◽  
Vol 20 (8) ◽  
pp. 1025-1030
Author(s):  
Daniel Levin ◽  
Arnan Seginer
Keyword(s):  
Arbitrary Planform

Nonstationary nonlinear theory of a thin wing of arbitrary planform

1976 ◽  
Vol 9 (4) ◽  
pp. 583-589 ◽  
Author(s):  
S. M. Belotserkovskii ◽  
M. I. Nisht
Keyword(s):  
Nonlinear Theory ◽  
Thin Wing ◽  
Nonstationary Nonlinear Theory ◽  
Arbitrary Planform

Inclined Flat Punch of Arbitrary Shape on an Elastic Half-Space

1986 ◽  
Vol 53 (4) ◽  
pp. 798-806 ◽  
Author(s):  
V. I. Fabrikant
Keyword(s):  
Integral Representation ◽  
Half Space ◽  
Arbitrary Shape ◽  
Contact Problems ◽  
Elastic Half Space ◽  
Elastic Contact ◽  
Circular Sector ◽  
Flat Punch ◽  
Circular Segment ◽  
Arbitrary Planform

A new method is proposed for the analysis of elastic contact problems for a flat inclined punch of arbitrary planform under the action of a normal noncentrally applied force. The method is based on an integral representation for the reciprocal distance between two points obtained by the author earlier. Some simple yet accurate relationships are established between the tilting moments and the angles of inclination of an arbitrary flat punch. Specific formulae are derived for a punch whose planform has a shape of a polygon, a triangle, a rectangle, a rhombus, a circular sector and a circular segment. All the formulae are checked against the solutions known in the literature, and their accuracy is confirmed.

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