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- W2315487557 abstract "Complex configurations such as transonic transport aircrafts are well suited for testing modern tools of aircraft design. These tools are computer based systems as well as wind tunnel test devices. This paper reports about combining theoretical, numerical and experimental techniques to analyze and influence specific aerodynamic phenomena such as the flow quality in the wing root area. Large size wind tunnel models are needed to investigate the flow around such specific parts of the model. The aim of controlling transonic flow quality at the wing-body junction in a small wind tunnel has motivated the design for an incomplete and modular configuration. Specific devices are needed to simulate a lift distribution resulting from the complete model: Circulation Control Splitter Blades (CCSB) are replacing the wing tips. The investigated high wing configuration is a generic model for a new military transport aircraft. The model, called the DLR-F9, was tested at the transonic wind tunnel (TWG) at the DLR Gottingen. Results from numerical simulation and a first set of experiments using CCSB's are reported." @default.
- W2315487557 created "2016-06-24" @default.
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- W2315487557 date "1997-06-29" @default.
- W2315487557 modified "2023-09-26" @default.
- W2315487557 title "Using flow control devices in small wind tunnels" @default.
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- W2315487557 doi "https://doi.org/10.2514/6.1997-1920" @default.
- W2315487557 hasPublicationYear "1997" @default.
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