2 edition of Analysis of airfoil transitional separation bubbles found in the catalog.
Analysis of airfoil transitional separation bubbles
R. L. Davis
Published
1984
by National Aeronautics and Space Administration, Scientific and Technical Information Branch, National Technical Information Service] in Washington, D.C, [Springfield, Va
.
Written in English
Edition Notes
| Statement | R.L. Davis and J.E. Carter ; prepared for Langley Research Center under contract NAS1-16585 |
| Series | NASA contractor report -- 3791 |
| Contributions | Carter, J. E, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center |
| The Physical Object | |
|---|---|
| Pagination | iii, 68 p. : |
| Number of Pages | 68 |
| ID Numbers | |
| Open Library | OL14931325M |
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An acoustic source is used to control the size and location of the laminar separation bubble on a FX airfoil. This is an alternative to reduce the negative bubble effects on the performance. Transitional separation bubbles and unsteady aspects of aerofoil stall Article in Aeronautical Journal -New Series- () July with 66 Reads How we measure 'reads'.
3 Laminar Separation Bubbles and Transition Low Reynolds number airfoil flows from DAMEC at Federal University of Technology.
American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA I was trying to simulate laminar bubble over naca using ANSYS Fluent with Transition SST model. My flow conditions are Re=, Turbulent. National Aeronautics and Space Administration VSP Aircraft Analysis User Manual • XFOIL is primarily used to collect profile drag data under various flight conditions.
–Max cruise, best endurance cruise, best climb and high lift scenarios. • Also used to determine a rough estimation of ideal CLmax (VSPAERO has none).
