aspect ratio - Globe Thesis

Keyword [aspect ratio] Result: 1 - 20 \| Page: 1 of 10
1.	Research On Semi-active Flutter Suppression Using Stepped Magnetorheological Dampers
2.	Investigation Of The Ignition Transient In Large Aspect Ratio Solid Rocket Motors
3.	Experimental Study On Punching Shear Strength Of RC Slabs With The Effect Of Column Aspect Ratios And Flexural Reinforcement Ratios
4.	Structure Optimization And Performance Analysis Of Axial-magnetized Permanent Magnet Micromotor Based On MEMS Technology
5.	Research On Seismic Performance Of Steel Reinforced Concrete Frame-reinforced Concrete Core Wall Hybrid Structure In High Seismic Intensity Region
6.	Numerical Research On Three-dimensional Unsteady Flow Field Of Micro Air Vehicle And Aerodynamic Optimization
7.	Numerical Simulation Of Aerodynamic Characteristics For Micro Air Vehicles
8.	Optimum Design And Study On The Rotor Blades For Horizontal Axis Wind Turbines Generator System
9.	Research On Flow Characteristics And Control Rules Of Rectangular Isolators
10.	Research On Effective Reinforcement Arrangement And Analytical Model Of Coupling Beams With Small Aspect Ratio In Seismic Shear Walls
11.	Experimental Study On Short-span Coupling Beams With Efficacious Detailing
12.	Nonlinear Aeroelastic Response And Flutter Analysis Of High-Aspect-Ratio Wings
13.	Study On Rational Structural Design Of Staggered Truss System And Push-over Analysis
14.	Simulation For Identification Of Flutter Derivatives For Aerofoil Using Forced Vibration Method And Its Application
15.	Semi-Active Flutter Suppression Of A Wing Using Magnetorheological Dampers
16.	Experimental Investigation Of Flow And Heat Transfer In Microchannels
17.	Experimental Study On Reactive Powder Concrete With Environment-protecting And Energy-saving Properties
18.	Study On Solar Air Collector With Transparent Honeycomb Made Of Glass Tube
19.	Numerical Investigation On The Aerodynamic And Infrared Radiation Characteristics Of Spherical Convergent Flap Nozzles
20.	Research On The Effect Of Aspect Ratio On 2-D Hypersonic Inlet Performance
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