Loading...
Please wait, while we are loading the content...
Similar Documents
Flight investigation of stall, spin and recovery characteristics of a low-wing, single-engine, t-tail light airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Patton Jr., J. M. Stough II, H. P. Dicarlo, D. J. |
| Copyright Year | 1985 |
| Description | Flight tests were performed to investigate the stall, spin, and recovery characteristics of a four-place, low-wing, single-engine, T-tail, general aviation research airplane at an aft center-of-gravity position. Most stalls resulted in roll-offs. Spins were oscillatory in roll and pitch at 43 deg angle of attack; the magnitude of the oscillations was determined by aileron position. Power, flap deflection, and landing gear position did not affect the angle of attack to the spin. Antispin rudder followed by forward wheel with ailerons neutral produced the fastest and most consistent recoveries but the initial application of recovery controls did not always stop a spin. |
| File Size | 6756639 |
| Page Count | 97 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850016937 |
| Archival Resource Key | ark:/13960/t85j2dg9d |
| Language | English |
| Publisher Date | 1985-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Flight Tests Spin Dynamics Damage Assessment Angular Momentum Aeronautics Aircraft Performance Controllability Angle of Attack Aerodynamic Characteristics Aerodynamic Stalling Aircraft Spin Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
