Vacuum plume aerodynamic force measuring system and method
A vacuum and power technology, applied in the vacuum plume aerodynamic measurement system and measurement field, can solve the problem of no large-scale vacuum plume effect experimental system, and achieve the effect of avoiding errors and accurate measurement
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[0032] The present invention will be further described in detail below with reference to the drawings and embodiments.
[0033] The invention is a vacuum plume aerodynamic measurement system and measurement method.
[0034] The vacuum plume aerodynamic measurement system of the present invention is such as figure 1 As shown, it includes a vacuum chamber 1, an engine 2, a force measurement model 3, a plume protection cover 4, a displacement mechanism 5, a mounting base 501, and a six-component balance force measurement system 600.
[0035] The six-component balance force measurement system 600 includes a six-component balance 601, an in-cabin power supply cable 602, a power supply cable penetrating flange 603, an external power supply cable 604, a DC stabilized power supply 605, and an in-cabin signal cable 606, a signal conversion module 607, an in-cabin signal cable 608, a signal cable penetration flange 609, an out-of-cabin signal cable 610, and a data acquisition system 611.
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