Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Methods and systems for enabling wind tunnel models to transition between measuring aerodynamic forces and measuring acoustic signatures

Methods and systems for enabling wind tunnel models to transition between measuring aerodynamic forces and measuring acoustic signatures

US Patent 9134195 · Granted Sep 15, 2015

Estimated economic value: $19,814,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Wing, aircraft, and method for delaying wing stall of an aircraft2022
Drag reduction device for exposed landing gear cavities2020
Apparatus and method for reducing a sonic boom signature2018
Flow inlet2018
Supersonic elliptical ramp inlet2016
Correction of pressure signals measured during supersonic wind tunnel testing2014
Integrated high-speed aircraft and associated methods of manufacture2005
Aircraft support pylon1998