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A survey of active controls benefits to supersonic transports
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pratt, K. G. |
| Copyright Year | 1976 |
| Description | Results are drawn from studies of the impact of advanced technologies on the design of an arrow-wing configuration. Information presented includes estimated benefits, effects of combinations of active control concepts, and constraints. Emphasis is placed on characteristics that are uniquely related to a large airframe featuring a slender body with a fixed wing of low aspect ratio, high sweep, and small thickness ratio. |
| File Size | 1066148 |
| Page Count | 21 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760024073 |
| Archival Resource Key | ark:/13960/t0vq7qk74 |
| Language | English |
| Publisher Date | 1976-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Arrow Wings Aerodynamic Configurations Cost Effectiveness Fixed Wings Control Equipment Aircraft Design Supersonic Transports Slender Bodies Thickness Ratio Aircraft Control Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |