Method for machining lip of hypersonic-speed low-noise wind tunnel nozzle
The invention discloses a method for machining a lip of a hypersonic-speed low-noise wind tunnel nozzle. The method includes the following steps that clamping is carried out, the thickness of the lipworkpiece is measured and the length L of the lip is determined, steps of the length L of the lip are...
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Format: | Patent |
Sprache: | chi ; eng |
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