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Calculation of aerodynamic characteristics at high angles of attack for airplane configurations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Tseng, J. B. Lan, C. Edward |
| Copyright Year | 1987 |
| Description | The primary objective is to determine how an airplane configuration should be modeled to predict both longitudinal and lateral aerodynamic characteristics at high angles of attack. A generic fighter model, an F-16 and an F-18 configuration with leading edge flap deflection and an F-106B configuration were investigated. Furthermore, the F-16XL and X-29 configurations were examined. Some calculated results are given. |
| File Size | 480596 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870017427 |
| Archival Resource Key | ark:/13960/t2993464n |
| Language | English |
| Publisher Date | 1987-02-24 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics X-29 Aircraft Aerodynamic Configurations Leading Edge Flaps Computation F-106 Aircraft F-16 Aircraft F-18 Aircraft Angle of Attack Aerodynamic Characteristics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
