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Overview of the langley viscous drag reduction program
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hefner, Jerry N. |
| Copyright Year | 1986 |
| Description | As a result of reductions in form drag and roughness drag, skin friction, drag, or viscous drag now represents a major contributor to the cruise drag of subsonic business and transport aircraft, and hence, is considered a barrier problem to further significant improvements in the aerodynamic efficiency of these aircraft. To meet the challenge, research in the areas of laminar-flow control and turbulence control/drag reduction was initiated at NASA Langley Research Center. The significance of this research is discussed. |
| File Size | 266358 |
| Page Count | 7 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880005564 |
| Archival Resource Key | ark:/13960/t21c6vw2p |
| Language | English |
| Publisher Date | 1986-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Turbulent Flow Drag Reduction Laminar Flow Skin Friction Reynolds Number Fuel Consumption Boundary Layer Transition General Overviews Vortex Breakdown Aircraft Design Boundary Layer Control Data Bases Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |