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High lift selected concepts
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Henderson, M. L. |
| Copyright Year | 1979 |
| Description | The benefits to high lift system maximum life and, alternatively, to high lift system complexity, of applying analytic design and analysis techniques to the design of high lift sections for flight conditions were determined and two high lift sections were designed to flight conditions. The influence of the high lift section on the sizing and economics of a specific energy efficient transport (EET) was clarified using a computerized sizing technique and an existing advanced airplane design data base. The impact of the best design resulting from the design applications studies on EET sizing and economics were evaluated. Flap technology trade studies, climb and descent studies, and augmented stability studies are included along with a description of the baseline high lift system geometry, a calculation of lift and pitching moment when separation is present, and an inverse boundary layer technique for pressure distribution synthesis and optimization. |
| File Size | 4608471 |
| Page Count | 109 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19820007144 |
| Archival Resource Key | ark:/13960/t7wm6378h |
| Language | English |
| Publisher Date | 1979-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Airfoil Profiles Drag Reduction Transport Aircraft Flaps Control Surfaces Wind Tunnel Tests Stability Augmentation Pressure Distribution Aerodynamic Coefficients Aircraft Design Aspect Ratio Computer Aided Design Lift Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
