Зниження впливу нагріву поверхні фотоелемента на продуктивність його роботи
ВИЗНАЧЕННЯ ОПТИМАЛЬНОЇ МАСИ СОРБЕНТУ «ЕКОЛАН» ДЛЯ ОЧИЩЕННЯ ВОДИ ВІД НАФТОПРОДУКТІВ
Аналіз концепції об’єкта польотної інформації
Zeta potential measurement of bubbles in DAF process and its effect on the removal efficiency
Year in Review: Progress towards Decarbonizing Transport and Near-Zero Emissions
Year 2015 Transportation Plan. HATS (Huntsville Area Transportation Study)
X-HALE: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests
Worm wheel mechanism with passive rollers
Working Together on Transportation Planning: An Approach to Collaborative Decision Making
Work Analysis and Labour Productivity Evaluation Criteria
Wing Tip Vortices from an Exergy-Based Perspective
Wing Planform Geometry Effects on Large Subsonic Military Transport Airplanes
Wing Kinematics Optimization for Hovering Micro Air Vehicles Using Calculus of Variation
Wing body junctions in ship hydrodynamics
Wind-tunnel Tests of Single- and Dual-rotating Tractor Propellers of Large Blade Width
Wind-tunnel Tests of Single- and Dual-rotating Pusher Propellers Having from Three to Eight Blades
Wind-tunnel Tests of Four Curtiss Propellers Embodying Different Blade Sections
Wind-tunnel Tests of Eight-blade Single and Dual-rotating Propellers in the Tractor Position
Wind-tunnel Tests of a Dual-rotating Propeller Having One Component Locked or Windmilling
Wind Tunnel Testing of a 6%-Scale Large Civil Tilt Rotor Model in Airplane and Helicopter Modes
Wind-Tunnel Study of Gurney Flaps Applied to Micro Aerial Vehicle Wing
Wind-Tunnel Results of Advanced High-Speed Propellers at Takeoff, Climb, and Landing Mach Numbers
Wind Tunnel Investigations on Thin Supercritical Airfoils in the High Subsonic Flow Regime
Wind Tunnel Investigation of Rotor Lift and Propulsive Force at High Speed. Test Data Appendix
Wind Tunnel Investigation of Rotor Lift and Propulsive Force at High Speed: Test Data Appendix
Wind-tunnel Investigation of Ailerons on a Low-drag Airfoil III : the Effect of Tabs
Wind Tunnel Investigation of a Circulation Control Wing with Dual-Radius Flaps