CN112098036A
|
|
Interference force calibration device and method for wind tunnel test blade supporting device
|
CN112238932A
|
|
Aircraft flutter suppression device and aircraft thereof
|
CN112124562A
|
|
Aircraft and aircraft control method thereof
|
CN112098035A
|
|
Aircraft test system
|
CN111999030A
|
|
Three-dimensional oil flow VR (virtual reality) online measurement and display system and working method thereof
|
CN112014064A
|
|
Wind tunnel complex flow color fluorescent oil flow test method
|
CN112001991A
|
|
High-speed wind tunnel dynamic oil flow map image processing method
|
CN112268676A
|
|
Supersonic wind tunnel model pitching motion protection device
|
CN112268675A
|
|
Intelligent false strut device for high-speed wind tunnel
|
CN112229598A
|
|
Water-cooling support rod and machining method thereof
|
CN112268677A
|
|
Forced rock test device for high-speed wind tunnel
|
CN112230669A
|
|
Method for judging influence of pitching rate of aircraft on rolling motion stability
|
CN112268678A
|
|
Free rock test device for high-speed wind tunnel
|
CN112268682A
|
|
Method for predicting single-degree-of-freedom rock-roll characteristic of aircraft
|
CN112229597A
|
|
Tracer particle generator for large-scale high-speed wind tunnel PIV test
|
CN112197934A
|
|
Tracer particle concentration control method for large-scale high-speed wind tunnel PIV test
|
CN112179611A
|
|
Device for generating large-scale high-speed wind tunnel PIV tracer particles and remotely controlling flow
|
CN112171628A
|
|
Device for replacing solid spray pipe of high-speed wind tunnel
|
CN112171203A
|
|
Machining method of microporous spray pipe
|
CN112113704A
|
|
Pressure-sensitive paint response time calibration method based on non-electric detonator driving type shock tube
|