CN112173074A
|
|
Reusable high-temperature speed reducing plate mechanism
|
CN112270037A
|
|
Height modeling and flow control method for embedded capsule spoiler under high Mach number
|
CN112163271A
|
|
Atmospheric parameter calculation method of atmospheric data sensing system
|
CN111994300A
|
|
Full-size aircraft flight quality evaluation method based on scaling model
|
CN111780941A
|
|
Aircraft force measurement test model and method
|
CN111679687A
|
|
Guide control integration method with falling angle constraint
|
CN111717404A
|
|
Oil tank thermal protection structure for high-speed aircraft and high-speed aircraft with oil tank thermal protection structure
|
CN111614038A
|
|
Cable abrasion-proof protection device
|
CN111537428A
|
|
Cable thermal protection performance test device
|
CN111458100A
|
|
Aircraft bottom resistance coefficient correction method
|
CN111413011A
|
|
Method for testing influence of high-temperature conduction of adhesive on temperature measurement of thermocouple
|
CN111458366A
|
|
Ablation thermal protection system structure pneumatic heat/heat transfer coupling analysis method
|
CN111503428A
|
|
Thermal bridge blocking structure
|
CN111595490A
|
|
Method for measuring influence of high-temperature gas effect on pneumatic heat
|
CN112193401A
|
|
Thermal protection method for front edge of hypersonic aircraft
|
CN111444651A
|
|
Intermittent welding seam strength evaluation method
|
CN111412887A
|
|
Attack angle and sideslip angle identification method based on Kalman filtering
|
CN111422383A
|
|
Dimension structure of separation actuating device
|
CN111425489A
|
|
Guiding and limiting structure
|
CN111409814A
|
|
Thermal bridge blocking structure for aircraft and preparation method thereof
|