Publication Date:
2019-06-27
Description:
A numerical technique is presented for the design of two-dimensional supercritical wing sections with low wave drag. The method is a design mode of the analysis code H which gives excellent agreement with experimental results and is widely used in the aircraft industry. Topics covered include the partial differential equations of transonic flow, the computational procedure and results; the design procedure; a convergence theorem; and description of the code.
Keywords:
AERODYNAMICS
Type:
NASA-CR-158840
,
COO-3077-158
Format:
application/pdf
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