Bleischwitz et al., 2015 - Google Patents
Aeromechanics of membrane wings in ground-effectBleischwitz et al., 2015
View PDF- Document ID
- 12146168548519278424
- Author
- Bleischwitz R
- De Kat R
- Ganapathisubramani B
- Publication year
- Publication venue
- 45th AIAA Fluid Dynamics Conference
External Links
Snippet
Wind tunnel experiments are conducted in ground-effect (GE) at a moderate Reynolds number of Re= 56,000, measuring rigid flat plates and membrane wings at ground clearances of the trailing edge from 1% to 200% chord length. A force transducer is used to …
- 239000012528 membrane 0 title abstract description 192
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
- Y02T50/16—Drag reduction by influencing airflow
- Y02T50/166—Drag reduction by influencing airflow by influencing the boundary layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air-flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
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