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Accession Number:
ADA191408
Title:
An Integral Equation for the Linearized Supersonic Flow Over a Wing
Corporate Author:
DAYTON UNIV OH RESEARCH INST
Report Date:
1988-02-01
Abstract:
In the first formulation. the integral equation for linearized steady supersonic flows appears in a form where it is necessary to approach the planform from above or below by a limiting process. In the present report, the problem is transformed analytically in such a manner that this limiting process no longer appears and that the resulting expressions are numerically tractable. It is believed that such a formulation gives more freedom to take the particularities of a given problem into account. The formulation is applied to compute the conical field which arises at the top of an airfoil. A possible numerical approach to the solution of the integral equation in the general case is described, but only in a rough outline.
Descriptive Note:
Interim rept. Nov 1986-Aug 1987
Supplementary Note:
DOI: 10.21236/ADA191408
Pages:
0102
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
F33615-86-C-3200
File Size:
2.80MB
