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Control-surface hinge-moment calculations for a high-aspect-ratio supercritical wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Perry II, B. |
| Copyright Year | 1978 |
| Description | The hinge moments, at selected flight conditions, resulting from deflecting two trailing edge control surfaces (one inboard and one midspan) on a high aspect ratio, swept, fuel conservative wing with a supercritical airfoil are estimated. Hinge moment results obtained from procedures which employ a recently developed transonic analysis are given. In this procedure a three dimensional inviscid transonic aerodynamics computer program is combined with a two dimensional turbulent boundary layer program in order to obtain an interacted solution. These results indicate that trends of the estimated hinge moment as a function of deflection angle are similar to those from experimental hinge moment measurements made on wind tunnel models with swept supercritical wings tested at similar values of free stream Mach number and angle of attack. |
| File Size | 1028455 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780023100 |
| Archival Resource Key | ark:/13960/t2s51g373 |
| Language | English |
| Publisher Date | 1978-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Slender Wings High Aspect Ratio Torque Transonic Flow Control Surfaces Trailing Edges Fuel Consumption Supercritical Wings Compressible Flow Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
