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Approximate neutral point of a subsonic canard aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Phillips, J. D. |
| Copyright Year | 1985 |
| Description | An approximate formula is derived for the position of the neutral point in canard aircraft. This formula accounts for the aerodynamic interference between the wing (rear wing) and the canard (forward wing). Topics covered include determination of the canard downwash derivative, determination of the canard and wing liftslopes including the aerodynamic interference, and calculation of the neutral point position. |
| File Size | 295473 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850016894 |
| Archival Resource Key | ark:/13960/t03z34q50 |
| Language | English |
| Publisher Date | 1985-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Reversed Flow Static Stability Canard Configurations Subsonic Flow Aerodynamic Interference Downwash Pressure Distribution Angle of Attack Longitudinal Stability Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |