Engineering, 13.07.2021 14:00, usabmx34
A symmetric biplane having forward / aft wedge angles 2° is placed in supersonic
flow as shown below.
Estimate the lift and drag of this configuration by using the idea of method of
characteristics. (Recall v±0=const on different direction i. e left or right running waves)
%3D
The wave pattern on the biplane is shown in dashed lines.
(v,0)»=(28,0)
Answers: 3
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Engineering, 04.07.2019 18:10, Larkinlover703
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A symmetric biplane having forward / aft wedge angles 2° is placed in supersonic
flow as shown belo...
Mathematics, 24.07.2020 03:01
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