Patent ID: 11933694
Assignee: UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE
Field: Computer technology (Electrical engineering)
Classification: CPC G | IPC G

Claim 7:
8. An instrumented wind tunnel for testing a test subject, said wind tunnel comprising:
an inlet, a test stage for receiving a test subject, an exhaust, all in mutual fluid communication; and
an instrumentation system comprising: at least two channels, each said channel comprising a sensor for attachment to a test subject, said sensor being configured to report test data to a respective IMNC having at least a quad core processor; each said IMNC being in communication with a common 10 Gb/s switch, said switch communicating with a respective 10 Gb/s Ethernet card for that channel, said Ethernet card being in communication with a plurality of submasters, each said submaster of said plurality being configured to receive and send said data at a rate of at least 10 Gb/s.