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Nonlinear aerodynamic wing design
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bonner, Ellwood |
| Copyright Year | 1985 |
| Description | The applicability of new nonlinear theoretical techniques is demonstrated for supersonic wing design. The new technology was utilized to define outboard panels for an existing advanced tactical fighter model. Mach 1.6 maneuver point design and multi-operating point compromise surfaces were developed and tested. High aerodynamic efficiency was achieved at the design conditions. A corollary result was that only modest supersonic penalties were incurred to meet multiple aerodynamic requirements. The nonlinear potential analysis of a practical configuration arrangement correlated well with experimental data. |
| File Size | 4535803 |
| Page Count | 79 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880004697 |
| Archival Resource Key | ark:/13960/t6m090g73 |
| Language | English |
| Publisher Date | 1985-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Wings Supersonic Aircraft Aerodynamic Configurations Efficiency Potential Theory Models Design Analysis Fighter Aircraft Nonlinear Systems Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
