CN112268684A
|
|
Variable azimuth angle surface pressure measuring system and method for low-speed wind tunnel rotor model
|
CN112197933A
|
|
Width-adjustable opening jet flow wind tunnel chamber and opening jet flow wind tunnel test method
|
CN112197713A
|
|
Device and method for synchronously measuring deformation and surface pressure of helicopter rotor blade
|
CN112197932A
|
|
Surface temperature correction method and measurement method for airplane anti-icing and deicing test model
|
CN112197721A
|
|
Water film thickness measuring method
|
CN112129485A
|
|
Single-vector loading method for wind tunnel mechanical balance
|
CN112113740A
|
|
Pressure measuring device, pressure measuring method and wind tunnel local airflow deflection angle measuring method
|
CN112098040A
|
|
Measuring device and measuring method for mounting angle of directional dynamic pressure probe
|
CN112066912A
|
|
Synchronous measurement method and measurement device for three-dimensional surface profile and surface pressure of model
|
CN112014063A
|
|
A stores pylon for wind-tunnel test
|
CN111999029A
|
|
Supporting device for propeller test
|
CN111929026A
|
|
Low-frequency pressure pulsation suppression method for wind tunnel 3/4 opening test section
|
CN111929025A
|
|
Hot gas supply system and method for anti-icing and deicing test
|
CN112291025A
|
|
Rotating signal equal-direction synchronous triggering acquisition method based on optical fiber slip ring
|
CN111929024A
|
|
Icing wind tunnel air intake and height simulation system and method
|
CN112229596A
|
|
Coaxial rigid rotor wing lift force offset wind tunnel test method and system
|
CN111795796A
|
|
Icing wind tunnel ice prevention and removal test method and system
|
CN112197826A
|
|
Air inlet mass flow measuring device and measuring method for aircraft engine
|
CN111811770A
|
|
Wind tunnel model supporting device and adapter based on internal balance
|
CN112211726A
|
|
Continuous air entraining system based on turbojet engine
|