Loading...
Please wait, while we are loading the content...
Aerodynamic characteristics of the standard dynamics model in coning motion at mach 0.6
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schiff, L. B. Jermey, C. |
| Copyright Year | 1985 |
| Description | A wind tunnel test was conducted on the Standard Dynamics Model (a simplified generic fighter aircraft shape) undergoing coning motion at Mach 0.6. Six component force and moment data are presented for a range of angle of attack, sideslip, and coning rates. At the relatively low non-dimensional coning rate employed (omega b/2V less than or equal to 0.04), the lateral aerodynamic characteristics generally show a linear variation with coning rate. |
| File Size | 2899697 |
| Page Count | 77 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850023781 |
| Archival Resource Key | ark:/13960/t1tf4pd5k |
| Language | English |
| Publisher Date | 1985-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Conical Bodies Aerodynamic Stability Rotation Yaw Sideslip Pitch Wind Tunnel Tests Aircraft Maneuvers Mathematical Models Roll Angle of Attack Stability Derivatives Nonlinear Systems Aerodynamic Stalling Hysteresis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
