To determine the characteristics of new suction concepts for hybrid laminar flow control (HLFC) a modular flat plate wind tunnel model is investigated in the DNW-NWB wind tunnel facility. This approach allows detailed examination of suction characteristics in consideration of realistic boundary layer flow conditions. The following evaluation reveals the effects of joining methods between successive panels and other surface disturbances of porous materials and underlying chambers on HLFC techniques. After successful measurements with {and without} suction panels, this paper compares experimental results with theoretical and numerical approaches and draws conclusions from N-factor results and boundary layer (BL) measurements
Wind tunnel and flight tests have clearly demonstrated the potential of hybrid laminar flow control ...
The paper deals with the aerodynamic design of laminar flow wings. The main design concepts at prese...
Rise in the performance and therefore profit of airliners is a major challenge for aircraft designer...
The application of Hybrid Laminar Flow Control (HLFC) by suction of the boundary layer has the poten...
In the low speed wind tunnel Braunschweig (DNW-NWB), several measurement campaigns with sucked bound...
Current designs for Hybrid Laminar Flow Control (HLFC) systems on aircraft wings often feature passi...
Current designs for Hybrid Laminar Flow Control (HLFC) systems on aircraft wings often feature passi...
The aeroelastic assessment of hybrid laminar flow control systems for transport aircraft requires we...
A description is given of the development of, and results from, the hybrid laminar flow control (HLF...
For a simplified but effective suction chamber concept for hybrid laminar flow control by boundary-l...
Numerical approach of hybrid laminar flow control (HLFC) is investigated for the suction hole with a...
AbstractNumerical approach of hybrid laminar flow control (HLFC) is investigated for the suction hol...
The NASA/Boeing hybrid laminar flow control (HLFC) experiment, designed during 1993-1994 and conduct...
A wind-tunnel experiment on laminar flow control by suction at Mach 2 has been performed for an infi...
Hybrid laminar flow control (HLFC) can be a possible solution for future sustainable energy-efficien...
Wind tunnel and flight tests have clearly demonstrated the potential of hybrid laminar flow control ...
The paper deals with the aerodynamic design of laminar flow wings. The main design concepts at prese...
Rise in the performance and therefore profit of airliners is a major challenge for aircraft designer...
The application of Hybrid Laminar Flow Control (HLFC) by suction of the boundary layer has the poten...
In the low speed wind tunnel Braunschweig (DNW-NWB), several measurement campaigns with sucked bound...
Current designs for Hybrid Laminar Flow Control (HLFC) systems on aircraft wings often feature passi...
Current designs for Hybrid Laminar Flow Control (HLFC) systems on aircraft wings often feature passi...
The aeroelastic assessment of hybrid laminar flow control systems for transport aircraft requires we...
A description is given of the development of, and results from, the hybrid laminar flow control (HLF...
For a simplified but effective suction chamber concept for hybrid laminar flow control by boundary-l...
Numerical approach of hybrid laminar flow control (HLFC) is investigated for the suction hole with a...
AbstractNumerical approach of hybrid laminar flow control (HLFC) is investigated for the suction hol...
The NASA/Boeing hybrid laminar flow control (HLFC) experiment, designed during 1993-1994 and conduct...
A wind-tunnel experiment on laminar flow control by suction at Mach 2 has been performed for an infi...
Hybrid laminar flow control (HLFC) can be a possible solution for future sustainable energy-efficien...
Wind tunnel and flight tests have clearly demonstrated the potential of hybrid laminar flow control ...
The paper deals with the aerodynamic design of laminar flow wings. The main design concepts at prese...
Rise in the performance and therefore profit of airliners is a major challenge for aircraft designer...