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The longitudinal equations of motion of a tilt prop/rotor aircraft including the effects of wing and prop/rotor blade flexibility
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Curtiss Jr., H. C. |
| Copyright Year | 1976 |
| Description | The equations of motion for the longitudinal dynamics of a tilting prop/rotor aircraft are developed. The analysis represents an extension of the equations of motion. The effects of the longitudinal degrees of freedom of the body (pitch, heave and horizontal velocity) are included. The results of body freedom can be added to the equations of motion for the flexible wing propeller combination. |
| File Size | 7902152 |
| Page Count | 64 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760021138 |
| Archival Resource Key | ark:/13960/t8kd6pd7q |
| Language | English |
| Publisher Date | 1976-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Propeller Blades Helicopters Flexible Wings Pitch Bending Equations of Motion Flexibility Longitude Rotary Wings 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 |
