Supersonic flow and wing‐body interference
作者:
D. S. Jones,
期刊:
Mathematika
(WILEY Available online 1967)
卷期:
Volume 14,
issue 1
页码: 68-93
ISSN:0025-5793
年代: 1967
DOI:10.1112/S0025579300008032
出版商: London Mathematical Society
数据来源: WILEY
摘要:
SummaryThe velocity potential near the boundary of the disturbance is determined for steady supersonic flow past a simple body‐and‐wing model. It is found that the disturbance decays exponentially as it spreads round the body; the alteration caused by changing the radius of curvature is discussed. A universal formula for the potential away from the fuselage is also derived.
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